TELEMEURING DATA COMMUNICATION RELAY PLATFORM FROM ONE OR MORE SATELLITE SATELLITE (S) OF OBSERVATIO

专利摘要:
A communications relay platform of a space observation system, aboard an aircraft (34) moving above the clouds, includes a first receiving interface (104) for demodulating telemetry data from least one observing traveling satellite (4, 6), a second transmitting interface (108) for modulating and transmitting the received data to at least one destination ground station (12, 14, 16). The relay platform comprises a first downlink dual decryption / encryption chain (204) of telemetry data repatriated from at least one traveling observation satellite (4, 6) to the destination ground station (s) (4). 12, 14, 16).
公开号:FR3060246A1
申请号:FR1601749
申请日:2016-12-08
公开日:2018-06-15
发明作者:Francis Martinerie；Herve Sainct；Serge Taride；Jean Didier Gayrard
申请人:Thales SA；
IPC主号:

专利说明:

Holder (s): THALES.
Extension request (s)
Agent (s): MARKS & CLERK FRANCE General partnership.
RELAY PLATFORM FOR TELEMETRY DATA COMMUNICATION FROM ONE OR MORE OBSERVATION SATELLITE (S) SCROLLING TO THE GROUND.
FR 3 060 246 - A1
A communications relay platform for a space observation system, on board an aircraft (34) operating above the clouds, comprises a first reception interface (104) for demodulating telemetry data from at least at least one moving observation satellite (4, 6), a second transmission interface (108) for modulating and transmitting the data received to at least one destination ground station (12, 14, 16).
The relay platform comprises a first decryption / encryption chain with double descending level (204) of telemetry data repatriated from at least one observation satellite passing by (4, 6) towards the destination ground station or stations ( 12, 14, 16).
DATA COMMUNICATION RELAY PLATFORM
TELEMESURES FROM ONE OR MORE OBSERVATION SATELLITE (S) MOVING DOWN TO THE GROUND
The present invention relates to communications platforms serving as high speed data transmission relays between one or more traveling observation satellites, ie non-geostationary, and one or more ground station (s) for receiving said observation data, called thereafter telemetry data from observation satellites.
The present invention also relates to observation systems using such communication platforms as relays.
It is known that one of the factors limiting observation systems by non-geostationary moving satellites is the ability of the downward path of a moving satellite to descend to the receiving ground station or stations all the images taken by the satellite when said traveling satellite passes over said receiving ground station in geometric visibility with respect to said satellite.
In order to increase the capacity of the downlink of each of the traveling satellites, satellite observation systems have seen in recent decades an escalation in the frequencies used for downlinks, now progressing towards the X and Ka bands, so as to be able to route and descend more and more image data during the same time the satellite is visible in the station.
The current projects aim to continue this progression towards the optical frequencies which would make it possible to download even more telemetry data in the same lapse of time of overflight of the ground station of reception by the satellite.
However from very high frequency radio bands, that is to say above the UHF band, the attenuation due to the presence of clouds in the atmosphere results in a significant limitation of the bit rate, and this attenuation becomes prohibitive for optical links.
One solution allowing the use of higher frequencies on the downlink consists in using a communication relay platform, on board an aircraft, for example a drone or a balloon, operating at high altitude above the clouds, which eliminates the crippling attenuation of a radio signal caused by clouds, which only intervene in the retransmission between the communication platform and the receiving ground station, which retransmission takes place over a distance much shorter (a few kilometers to a few tens instead of several hundreds to thousands of kilometers) and in a place allowing the use of specific allocations of frequencies and transmission bands, with the major advantage of being able to be permanent.
Despite the existence of regulatory requirements for the bands usable between high altitude relays and the ground and even if these bands are not necessarily advantageous in terms of accessible speed, these usable bands are less congested than the bands allocated to satellites .
The use of a high altitude relay as a relay between the ground and the traveling satellites is very interesting: since the relay is above the clouds, a downlink optical link between the traveling satellite and the high altitude relay platform allows communications broadband with 100% availability during the passage of the satellite in relay visibility, typically a few minutes to ten minutes for satellites in low orbit. The second downlink between the relay platform and the receiving ground station can be achieved by radio frequency in a frequency band less sensitive to clouds and precipitation, with a lower flow compensated by permanent visibility. While a passing observation satellite can be seen from a ground station approximately 40 minutes a day, the high altitude relay allows a gain of more than a factor of 30 in the flow requirement from the relay station to the ground.
The patent application US Pat. No. 6,151,308 A describes a satellite system using high-altitude relay platforms which make it possible to define communications cells more precisely, to avoid obstructions in the satellite links between the terminals and the traveling satellites at low orbit, especially when the terminals are located in an urban environment, and thus allow the access of a greater number of terminals to the network of the communications system. The patent application US 6,151,308 A describes an advantageous use of the satellite system within the framework of an observation mission which makes it possible to obtain finer and better resolution images by embedding the observation instruments on the relay platforms. at high altitudes instead of moving satellites. The document US Pat. No. 6,151,308 A does not describe the use of a communication relay platform to facilitate the repatriation of large telemetries from traveling observation satellites and does not describe how transmission security is managed at the satellite system. observation, and in particular at the level of the communications relay platform, in the case of relays with a multiplicity of satellites and / or multiple receiving ground stations.
A first technical problem is to provide an architecture for integrating security functions, at the level of the satellite observation system and in particular at the level of the communications relay platform, which simplifies the management of transmission security in the case a multiplicity of multiple receiving satellites and / or ground stations.
A second technical problem is to increase the availability and the capacity of the downlink from the relay platform to the ground station to remedy a crippling drop in speed or an absence of downlink between the relay platform and the ground station, caused for example by the interposition of very absorbent clouds vis-à-vis the radiation.
To this end, the subject of the invention is a communication relay platform for a space observation system, configured to be carried on board an aircraft flying above the clouds, and configured to serve as a high altitude relay. for transmission at high speed of spatial observation data, called telemetry, between at least one non-geostationary passing observation satellite and at least one ground station of destination and reception of said data, the transmission from the satellite or satellites observation to the high altitude relay which can take place in one or more predetermined visibility windows of the observation satellite or satellites parading towards the aircraft, and the transmission of data from the aircraft to the ground which can take place permanently. The relay platform comprises a first receiving antenna, configured to receive observation data, in a first optical or radiofrequency band, transmitted over a first downlink wireless spatial link, connecting at least one passing observation satellite to the platform. relay, and a first reception interface, connected to the first reception antenna and configured to demodulate the data received by the first antenna and save them in a memory, and a second transmission interface, configured to modulate the observation data stored in the memory, and transmit in a second radiofrequency band said modulated data via a second transmit antenna on a second downlink wireless aerial link directly connecting the relay platform to at least one destination ground station. The relay platform is characterized in that it comprises a first double-level decryption / encryption chain descending from telemetry data retrieved from at least one observation satellite parading towards the destination ground station or stations.
According to particular embodiments, the communication relay platform includes one or more of the following characteristics:
.- the first frequency band of the first downlink wireless space link is an optical or radio frequency band, and / or the second frequency band of the second downlink air link is an optical or radio frequency band;
.- the relay platform further comprises a third reception interface, configured to demodulate data from secure remote controls of the relay platform and / or of the passing satellite (s) of observation, prepared and transmitted over a third dedicated link by a ground control center of the space observation system;
.- the first descending double level decryption / encryption chain is configured:
. * for each passing observation satellite and the corresponding received telemetry data, decrypt at a first down level said telemetry data, encrypted and transmitted by said observation satellite traveling on the first downward space link and demodulated by the first interface , using active decryption keys of the data of the descending first level telemetry data, associated with said traveling satellite and of active key indices of encryption / decryption of the descending first level telemetry data, said active key indices of 'Encryption / decryption being transmitted jointly with said encrypted telemetry data and being associated in a unique manner with said moving observation satellite and with said active decryption keys of first descending level; then. * for each destination ground station and the corresponding telemetry data intended for them, decrypted at the first descending level and coming from one or more observation satellites, encrypt at a second descending level the telemetry data decrypted at the first descending level using an active encryption key for second descending telemetry data, associated with said destination ground station, and adding to said encrypted second descending data an index of active encryption / decryption key for telemetry data second down level, uniquely associated with said destination ground station and said active second down level encryption key;
the first double-level decryption / encryption chain descending telemetry data, brought back from the satellite (s) parading towards the destination ground station (s), comprises a first key management module encryption / decryption of the double descending level, a second decryption module at a first descending level of the telemetry data, transmitted on the first spatial downlink and demodulated by the first interface, and a third encryption module at a second descending level of the telemetry data decrypted at the first descending level; and the first module for managing the descending double level encryption / decryption keys of the telemetry data is configured to initially receive a first set of one or more sets of descending first level telemetry decryption keys, and to initially receive a second set of one or more sets of encryption keys for descending second level telemetry data; and each set of telemetry decryption keys relating to the first downlink level is associated with a moving observation satellite, and each telemetry decryption key relating to the first downlink level of each set is matched to and uniquely identified by a first descending level encryption / decryption key index; and each set of telemetry data encryption keys for the second downlink level is associated with a destination ground station, and each telemetry data encryption key for the second downlink level of each set is matched and uniquely identified by a second descending level encryption / decryption key index;
the first module for managing the encryption / decryption keys with double level descending telemetry data is configured to execute, upon reception via the third dedicated remote controls interface, secure and sent by the terrestrial control center, modifications of a part or all of the decryption keys of the telemetry data at the first down level and / or the encryption keys of telemetry data at the second down level;
the first reception antenna, the first reception interface, and the memory are configured to receive, demodulate and save separately telemetry data, encrypted at the first descending level and transmitted by at least two non-geostationary moving observation satellites on the first downlink space link, and / or the second transmit antenna, the second transmit interface, are configured to separately modulate and transmit the encrypted telemetry data at the second downlink level to at least one destination ground station on the second air link wireless downlink; and the first double-level decryption / encryption chain descending from telemetry data, repatriated from the satellite (s) parading towards the destination ground station (s), comprises a matrix allocator of decrypted telemetry, received from the same passing observation satellite, at different destination ground stations, according to an allocation table loaded by remote controls, the matrix allocator being connected in series between the second decryption module and the third encryption module;
the relay platform further comprises a second double-level decryption / encryption chain amounting remote control data from the observation satellite or satellites received via the third reception interface of the third dedicated remote control link secured from the ground control center;
the second double-level decryption / encryption chain amount of remote control data from the scrolling observation satellite (s) is configured;
. * for each observation satellite passing by the destination and the remote control data of said corresponding satellite, decrypt at a first level the remote control data, transmitted by the terrestrial control center on the third link and demodulated by the third interface, using an active key for decrypting first level ascending remote control data, associated with said observation satellite and an active key index index / decrypting first level ascending remote control data, said active key encryption index / decryption of the remote control data being transmitted in conjunction with the remote control data encrypted by the terrestrial control center and being associated in a unique manner with the traveling satellite and with said first uplink decryption key; then. * for each scrolling observation satellite of destination and the decrypted remote control data intended for it, encrypt at a second level up the decrypted remote control data at the first level up using an active encryption key for the data second uplink remote controls, the active key for encryption of the second uplink remote control data being associated with the destination observation satellite, and add to said second uplink level remote control data, an active encryption key index / decryption of remote controls, associated uniquely with said observation satellite and with said active second level uplink encryption key;
.- the relay platform further comprises a fourth transmission interface, configured to modulate remote control data from at least one passing observation satellite, and transmit said modulated remote control data via a fourth transmission antenna on a fourth uplink wireless space link directly linking the platform platform to the passing observation satellite (s); and in which the second decryption / encryption double-level encryption chain of the remote control data of the observing satellite (s) comprises a fourth module for managing the encryption / decryption keys of the double ascending level, a fifth decryption module at a first uplink level of the remote control data, transmitted on the third link and demodulated by the third interface, and a sixth encryption module at a second uplink level of the remote control data decrypted at the first uplink level; and the fourth dual-level encryption / decryption key management module for the remote controls of the scrolling satellite (s) is further configured for:
. * initially receive a third set of one or more sets of decryption keys of first level remote controls, and. * initially receive a fourth set of one or more sets of encryption keys of second level control; and each set of remote control decryption keys for the first uplink level is associated with a scrolling observation satellite, and each remote control decryption key data for the first uplink level of each set is matched to and uniquely identified by a index key for encryption / decryption of remote control data at the first uplink level; and each set of remote control encryption keys for the second uplink level is associated with a scrolling destination observation satellite, each remote control encryption key for the second uplink level of each set is matched to and identified so unique by an encryption / decryption key index at the second rising level;
the fourth module for managing the encryption / decryption keys at double level of the remote control data of the moving satellite (s) is configured to execute, on reception via the third dedicated remote control interface, secured and sent by the terrestrial control center, modifications of part or all of the decryption keys of the remote control data at the first uplink level and / or the encryption keys of the remote control data on the second uplink level;
the relay platform further comprises a fifth transmission interface, configured to modulate the observation data stored in the memory, and transmit in a fifth optical or radiofrequency band said modulated data via a fifth transmission antenna on a fifth link wireless uplink space directly connecting the relay platform to a geostationary satellite, the memory being configured to route, in a piloted manner from the ground by sending a dedicated command, the telemetry data on the fifth transmission interface, instead of the second transmission interface taken as the destination port in a nominal mode.
The subject of the invention is also a space system comprising at least one non-geostationary passing observation satellite (s), at least one destination ground station (s) and for receiving transmitted observation data at a high speed by the at least one observation satellite, an aircraft operating at a high altitude exceeding that of the clouds, and a communications relay platform, on board the aircraft and serving as a data transmission relay observation or telemetry between the at least one observation satellite and the at least two destination and data reception ground stations, in which the communications relay platform is defined according to the characteristics described above, and l he aircraft is included in the assembly formed by drones, stratospheric airships or airplanes.
According to particular embodiments, the space system further comprises a geostationary satellite and at least one remote and remote ground station, connected to said geostationary satellite by a downward geostationary space link, and the relay platform comprises a fifth transmission interface. , configured to modulate the observation data stored in the memory, and transmit in a fifth optical or radio frequency band said modulated data via a fifth transmitting antenna on a fifth uplink spatial wireless link directly connecting the relay platform to a satellite geostationary, the memory being configured to route, in a piloted manner from the ground by sending a dedicated command, the telemetry data on the fifth transmission interface instead of the second transmission interface taken as destination port in a nominal mode.
The invention will be better understood on reading the description of several embodiments which follows, given solely by way of example and made with reference to the drawings in which:
Figure 1 is a general view of a space system according to the invention using a relay platform on board an aircraft piloted above the clouds;
.- Figure 2 is a view of the general architecture of the platform platform of the invention and its main interfaces with the other elements of the space observation system of Figure 1;
.- Figure 3 is a view of a first embodiment of a relay platform according to the invention, derived from the general architecture of Figure 2 which optimally integrates the safety functions concerning descent protection telemetry data from traveling observation satellites;
.- Figure 4 is a view of a second embodiment of the relay platform according to the invention, derived from the first embodiment of Figure 3, which also incorporates in addition security functions concerning uphill protection remote controls for scrolling observation satellites;
.- Figure 5 is a general view of the communications architecture of the space observation system of Figure 1, integrating the security functions and corresponding to the second embodiment of the relay platform of Figure 4, the platform - relays integrating the securing of telemetry and remote controls for scrolling observation satellites, and directly receiving remote controls for observation satellites from a ground control center;
Figure 6 is a view of a particular embodiment of the space system of Figure 1 which predominantly uses a relay platform, on board an aircraft piloted above the clouds, and incidentally a geostationary satellite as second relay;
.- Figure 7 is a view of the architecture of the relay platform of the invention and its main interfaces with the other elements of the space observation system of Figure 6;
.- Figure 8 is a view of a first communications architecture of the space observation system of Figure 6 in which the relay platform optimally integrates both the security functions relating to the protection of descent data from observation telemetry and security functions relating to the upward protection of remote controls for moving observation satellites;
FIG. 9 is a view of a second communications architecture of the space observation system of FIG. 6 in which the relay platform only integrates the securing of telemetry from the traveling observation satellites and serves only as a transparent relay to -vis the securing of remote control data from observation satellites;
Figure 10 is a view of a third communications architecture of the space observation system of Figure 6 in which the relay platform only integrates the securing of telemetry from the traveling observation satellites and does not participate in the transmission of data of remote controls from the ground control center to the scrolling observation satellites.
In general, a satellite observation system according to the invention uses a high altitude communications relay platform which is on board an aircraft flying above the clouds, for example a drone or a stratospheric balloon, and which allows to extend the ability to lower telemetry from traveling satellites to the ground of telemetry.
The relay platform is configured to relay the data directly to at least one destination ground station with permanent visibility of the aircraft, .- either with a speed identical to the speed of the downlink between the observation satellite and the platform - relay, .- either with a lower bit rate by means of a buffer memory on board the relay platform, which is achievable due to the orbital geometry of the traveling observation satellites which implies brief spaced download windows time out.
The result is an increase in potential throughput, and therefore in the observation service, for example imagery or other observation data (radar, RF radio frequency, etc.), of the order of 150% and which can exceed 1000%.
Furthermore, the relay platform can be used for contexts in which data from multiple satellites are transmitted to multiple ground stations.
The basic concept of the invention which solves the first technical problem, namely providing an architecture for integrating the security functions in the satellite observation system, simplified and compatible for transmissions in the case of satellite constellations and / or of multiple receiving ground stations, is based on maximizing the integration of security functions and managing the secure links of the space observation system within the communications relay platform.
According to FIG. 1 and an exemplary embodiment of the invention, a spatial observation system 2 comprises:
.- at least one non-geostationary passing observation satellite, here two observation satellites 4 and 6, .- at least two destination and reception ground stations 12, 14, 16 of observation data, transmitted at a rate raised by at least one observation satellite 4,6, .- a communications relay platform 32, on board an aircraft 34 and serving as a relay for transmission of observation data, also called telemetry here 'observation, between the at least one passing observation satellite (s) 4, 6 and the destination and reception ground stations 12, 14, 16 of the observation data, .- the aircraft 34 of transport of the relay platform 32, .- a first control center 46 of the relay platform 32, and .- a second control center 48 of the traveling observation satellites 4, 6.
Aircraft 34 is included in the assembly formed by drones, airships or airplanes. Here in Figure 1, the aircraft 34 shown is a stratospheric airship.
The aircraft 34 is configured and piloted to operate above the atmospheric water clouds, thus allowing the establishment of space links, descending from the observation satellites 4, 6 to the aircraft 34, and if necessary rising from the platform relay 32 to observation satellites 4, 6, for example in an optical band or an RF radio band at high frequencies.
The aircraft 34 is piloted above the clouds so as to be as close as possible and in optical visibility to the destination and reception ground stations 12, 14, 16, called “local stations”, and to avoid attenuations caused by elements. possible atmospheric such as atmospheric clouds.
In general, the atmospheric elements, forming a radiation screen, are mainly water clouds but can also be winds of sand, clouds of air pollutants depending on the terrestrial regions considered.
According to FIG. 2 and a general example of architecture of the relay platform according to the invention, the communication relay platform 32 of FIG. 1 is configured to be on board the aircraft 34, piloted to evolve over the above the clouds, and it is configured to withstand the environmental conditions associated with the environment in which the aircraft 34 evolves, for example the stratosphere for a stratospheric balloon.
The relay platform 32 is configured to serve as a relay for transmitting spatial observation or telemetry data at a high speed, between one or more non-geostationary traveling observation satellites, here the traveling observation satellites 4 and 6, and at least one ground station of destination and of reception of said data, here the ground stations of destination 12, 14, 16, the transmission taking place in one or more predetermined visibility windows of the scrolling observation satellite (s) 4, 6 vis- opposite the aircraft 34.
The communication relay platform 32 includes a first reception antenna 102, a first reception interface 104, a buffer memory 106, a second transmission interface 108, a second transmission antenna 110.
The first reception antenna 102 is configured to receive observation data, in a first optical or radio frequency band, transmitted over a first downlink wireless spatial link 122 connecting at least one traveling observation satellite to the relay platform 32.
The first reception interface 104, connected to the first reception antenna 102, is configured to demodulate the telemetry data received by the first antenna 102 and to save them in the memory 106.
The second transmission interface 108 is configured to modulate the observation or telemetry data stored in the memory 106, and transmit in a second radiofrequency band said modulated telemetry data via the second transmission antenna 110 on a second overhead link without downlink 128 “local”, directly connecting the relay platform 32 to at least one local destination ground station (s), here the local destination ground stations 12, 14 and 16.
The first frequency band of the first wireless spatial link 122 is an optical or radio frequency band, and / or the second frequency band of the second overhead link 128 is a radio frequency band.
According to FIG. 2, the relay platform 32 also includes a third reception interface 142, configured to receive through a third reception antenna 144 and to demodulate data from secure remote controls of the relay platform 32, prepared and transmitted on a third dedicated link 152 by the terrestrial control center 46 of the relay platform 32.
According to FIG. 3 and a first particular embodiment 202 of the relay platform 32 integrating the security functions, the platform platform 202 comprises a first decryption / encryption chain with double descending level 204 of observation or telemetry data, retrieved from at least one satellite moving towards the destination ground station or stations, here the challenging satellites 4 and 6.
The first descending double level decryption / encryption chain 204 is configured:
.- for each observation satellite traveling 4, 6 and the corresponding received telemetry data, decrypt at a first down level said telemetry data, encrypted and transmitted by said observation satellite traveling on the first downlink space link 122 and demodulated by the first interface 104, using an active decryption key for the descending first level telemetry data, associated with said traveling satellite and with an active key index for encryption / decryption of the descending first level telemetry data, said index active encryption / decryption key being transmitted together with said encrypted telemetry data and being uniquely associated with said traveling satellite and said active decryption key; then for each destination ground station 12, 14, 16 and the corresponding telemetry data intended for them, decrypted at the first down level and coming from one or more observation satellites 4, 6, encrypt at a second level down said telemetry data decrypted using an active downlink second level telemetry data encryption key associated with said destination ground station, and add to said second level encrypted data an active key encryption / decryption key data index second descending telemetry, uniquely associated with said destination ground station and said active encryption key.
It should be noted that sets of decryption and encryption keys, respectively of the first and second descending levels, and sets of telemetry key indices of the first and second associated levels are previously loaded in the decryption / encryption means. dual level 204 through the third reception interface 142 of the third dedicated link 152 of secure remote control from the first terrestrial control center 46. The activation of the keys is implemented within these sets of keys by remote controls indices of active keys.
The first descending double level decryption / encryption chain 204 of telemetry data, returned from the traveling satellite (s) 4, 6 to the destination ground station (s) 12, 14, 16, comprises a first module 212 for managing the encryption / decryption keys of the double downlink level, a second module 214 for decryption at a first downlink level of the telemetry data, transmitted on the first downlink space link 122 and demodulated by the first interface 104 , and a third encryption module 216 at a second down level of decoded telemetry data at the first down level.
The first module 212 for managing the dual level encryption / decryption keys descending from the telemetry data is configured to:
initially receive a first set of one or more sets of descending first level telemetry decryption keys; and .- initially receive a second set of one or more second level telemetry descending data encryption key sets.
Each set of telemetry decryption keys relating to the first descending level is associated with a scrolling observation satellite, and each telemetry decryption key relating to the first descending level of each set is paired with and uniquely identified by an index encryption / decryption key at the first descending level.
Each telemetry data encryption key set for the second downlink level is associated with a destination ground station, and each telemetry data encryption key for the second downlink level of each set is matched to and uniquely identified by a second descending level encryption / decryption key index.
The first module 212 for managing the encryption / decryption keys with double level descending telemetry data is configured to execute, on reception via the third interface 142 of dedicated remote controls, secured and sent by the first terrestrial control center 46, modifications of part or all of the decryption keys of the telemetry data at the first down level, and / or of the encryption keys of telemetry data at the second down level.
According to FIG. 3, the first reception antenna 102, the first reception interface 104, and the memory 106 are configured to receive, demodulate and save observation or telemetry data separately, encrypted at the first down level and transmitted by one or more several non-geostationary scrolling observation satellites, here observation satellites 4, 6, on the first downward space link 122.
The second transmitting antenna 110 and the second transmitting interface 108 are configured to modulate and transmit the encrypted telemetry data at the second downlink level to the destination ground station or stations 12, 14, 16 on the second wireless air link. descending 128.
The first descending double-level decryption / encryption chain 204 of telemetry data, returned from the traveling satellite (s) 4, 6 to the destination ground station (s) 12, 14, 16 comprises here a matrix allocator 224 of decrypted telemetry, received from the same passing observation satellite, at different destination ground stations, according to a predetermined allocation table 226.
The matrix allocator 224 is connected in series between the second descending first level decryption module 214 and the third descending second level encryption module 216.
The allocation table 226 is here a matrix with two lines and five columns for encoding a predetermined interconnectivity, fixed or modifiable by command, between the observation satellites and the destination ground stations, the line index encoding the rank j of the observation satellite and the column index encoding the rank k of the destination ground station.
According to a first variant, a broadcast to all the destination ground stations to all the data repatriated from the observation satellites can be implemented, sorting being carried out at the destination ground stations in this case.
According to a second variant, an instruction for allocating telemetry data, for example images, to such or such receiving ground station, is provided by being contained in the metadata associated with the images and therefore received with said images by the relay platform. This allows frame-by-frame allocation rather than satellite-to-satellite.
The second and third modules 214, 216 are connected to the first module 212 via bidirectional links and are configured to search there respectively for the active descending first level decryption key and the active descending second level encryption key as a function of the two. indices of corresponding active encryption / decryption keys received beforehand by remote control.
Several modes of memory management 106 are possible.
According to a first preferred mode of management of the memory 106, the encrypted data, brought back from the observation satellites 4, 6, are stored encrypted in the memory 106, then decrypted and encrypted before sending to the destination ground stations 12, 14 , 16.
According to a second mode of management of the memory 106, the encrypted data, brought back from the observation satellites 4, 6, are first decrypted, then stored decrypted in the memory 106, and then encrypted before sending to the ground stations of destination 12,14,16.
According to a third mode of management of the memory 106, the encrypted data, brought back from the observation satellites 4, 6, are successively decrypted and stored decrypted in the memory 106, then successively encrypted at the second descending level and stored encrypted in the memory 106 before sending to the destination ground stations 12, 14, 16.
According to Figure 4 and a second particular embodiment 252 of the relay platform 32, the relay platform 252 is derived from the first embodiment 202 of the relay platform and comprises the same components numbered identically, in particular the first double-level decryption / encryption chain descending 204 of the telemetry data, repatriated from at least one satellite parading towards the destination ground station or stations, here the challenging satellites 4 and 6.
The communications relay platform 252 further comprises a second double-level decryption / encryption chain 254 of the remote control data of the observing satellite (s), in this case the observation satellites 4, 6 , received via the third reception interface 142 of the fourth dedicated secure remote control link 152 coming from the first ground control center 46.
The second double-level decryption / encryption chain amounting to 254 of the remote control data of the orbiting observation satellite (s) is configured:
.- for each observation satellite passing by destination 4, 6, and the remote control data of said corresponding satellite, decrypting at a first level the remote control data transmitted by the first terrestrial control center 46 on the third link 152 and demodulated by the third interface 142, using an active key for decrypting first level remote control data, associated with said observation satellite and an index of active key for encrypting / decrypting first level remote control data, said active key encryption / decryption index index of the remote control data being transmitted jointly with the remote control data encryption by the first terrestrial control center 46 and being associated in a unique manner with the traveling satellite and with said active decryption key; then for each destination scrolling observation satellite 4, 6, and the decrypted remote control data intended for it, encrypting at a second rising level the remote control data decrypted at the first rising level using an active data encryption key second-level remote controls, the encryption key for second-level remote control data being associated with the destination observation satellite, and adding to said encrypted data of second-level remote controls, an active key decryption index of the remote control data, uniquely associated with said observation satellite and with said active second level uplink encryption key.
It should be noted that sets of decryption and encryption keys, respectively of the first and second uplink levels are previously loaded into the uplink double level decryption / encryption means 254 through the third reception interface 142 of the third 152 dedicated secure remote control link 152 from the first terrestrial control center 46. The activation of the keys is implemented via the key indices contained in remote controls.
According to Figure 4, the communications relay platform 252 also includes a fourth transmission interface 256, configured to modulate remote control data from at least one passing observation satellite (s), and transmit said modulated remote control data via a fourth transmitting antenna 258 on a fourth uplink space wireless link 260 directly connecting the relay platform 252 to the traveling observation satellite (s) 4 and 6.
The second double-level decryption / encryption chain up 254 of the remote control data of the observation satellite or satellites 4, 6 comprises a fourth module 262 for managing the encryption / decryption keys of the double level amount, a fifth module 264 decryption at a first level amount of the remote control data, transmitted over the third link 152 and demodulated by the third interface 142, and a sixth module 266 encryption at a second level amount of the remote control data decrypted at the first level rising.
The fourth module 262 for managing the two-level encryption / decryption keys amounting to the remote controls of the moving satellite (s) is configured to:
initially receive a third set of one or more sets of first level uplink remote control decryption keys, and initially receive a fourth set of one or more sets of second level uplink remote control encryption keys.
Preferably, the third set contains a unique set of decryption keys for first level remote controls so that the encryption of the third link 152 ground relay platform is independent of the observation satellites and that it is at the level of the relay platform that specialize satellite encryption. Thus, securing the first uplink is simpler to implement and made more robust.
As a variant, the third set contains several sets of decryption keys for first level remote controls. In this case, each set of remote control decryption keys relating to the first uplink level is preferably associated with a scrolling destination observation satellite, and each remote control decryption key to the first uplink level of each set is paired to and uniquely identified by an encryption / decryption key index of the remote control data at the first uplink level.
Each set of remote control encryption keys relating to the second uplink level is associated with a scrolling destination observation satellite, and each remote control encryption key relating to the second uplink level of each set is paired with and identified so unique by an encryption / decryption key index at the second rising level.
The fourth module 262 for managing the encryption / decryption keys at a double level amount of remote control data from the moving satellite (s) is configured to execute, upon reception via the third interface 152 of dedicated, secure and remote controls. sent by the first terrestrial control center 46, modifications of part or all of the decryption keys of the remote control data at the first uplink level and / or the encryption keys of remote control data at the second uplink level.
The fifth and sixth modules 264, 266 are connected to the fourth module 262 via bidirectional links and are configured to search there respectively for the active first level up decryption key and the active second level up encryption key as a function of the two. indices of corresponding active encryption / decryption keys received beforehand by remote control.
Several modes of memory management 106 are possible.
According to a first preferred mode of management of the memory 106, the encrypted data, brought back from the observation satellites 4, 6, are stored encrypted in the memory 106, then decrypted and encrypted before sending to the destination ground stations 12, 14 , 16.
According to a second mode of management of the memory 106, the encrypted data, brought back from the observation satellites 4, 6, are first decrypted, then stored decrypted in the memory 106, and then encrypted before sending to the ground stations of destination 12, 14, 16.
According to a third mode of management of the memory 106, the encrypted data, brought back from the observation satellites 4, 6, are successively decrypted and stored decrypted in the memory 106, then successively encrypted at the second descending level and stored encrypted in the memory 106 before sending to the destination ground stations 12, 14, 16.
In all cases, the remote control data, decrypted at the first uplink level of one or more traveling satellites contain the indices associated with the encryption key (s) of the descending first level telemetry data and the indices associated with the keys second level up encryption / decryption.
Only when the keys are updated, the remote control data, decrypted at the first uplink level associated with a moving observation satellite, contains the encryption keys for the telemetry data of the first downward space link, as well as the keys for decryption of the remote control data of the fourth uplink space link.
As a variant and in a particular way, a third embodiment of the relay platform is derived from the first embodiment 302. This third embodiment of the relay platform comprises the first decryption / encryption chain with double descending level 204 of the telemetry data described in Figure 3 but has no second double-level decryption / encryption chain amounting to remote control data from the moving observation satellites.
Thus, the use of a communications relay platform, on board an aircraft, included among drones, stratospheric airships and airplanes is able to provide a specific solution for securing data from observation, via the carrying out of routing and data encryption / decryption management functions, used by the various scrolling observation satellites and destination ground stations, via taking into account the management of encryption keys and / or decryption and decryption / encryption functions on board the relay platform
Thus, the security functions integrated at the level of a communication relay platform make it possible to simplify the management of the security of the transmissions in the case of the use of multiple satellite constellations and / or of multiple destination ground stations.
The security functions concerning key management, decryption / encryption of telemetry data from the scrolling satellites and the remote controls, if any, from the scrolling satellites allow:
.- the simplification of the management of the satellite keys, the transfer of the complexity of management of the satellites passing towards the aircraft, and of management of the satellite / ground links towards the links of the ground-drone control segment;
.- management from the relay platform of the security of several scrolling observation satellites, .- management on board the relay platform of the distribution of data from the same satellite, descended encrypted with a unique key, to multiple users with separate keys.
According to FIG. 5 and a communication architecture 302 of the observation system 2 of FIG. 1, the communication system 302 of the observation system uses a relay platform 252 according to the second embodiment of FIG. 4 which integrates with a high degree of security functions for telemetry and remote control data from observation satellites 4, 6.
In this architecture, the descent of secure telemetry from observation satellites to local destination stations 12, 14, 16 takes place via double-level links combining, as desired, a downlink of first-level telemetry 122-1 or 122 -2 and a downlink of second level telemetry taken from links 110-1, 110-2, and 110-3.
In this architecture, the rise of secure remote controls of the observation satellites, from the first terrestrial control center 46 to the observation satellites 4, 6 takes place via the relay platform 252 through double-level links combining at choice the first uplink 152 of the first level and a connection 260-1 or 260-2 of the double uplink of second level remote controls.
According to FIG. 6 and a variant 312 of the space observation system 2 of FIG. 1, the space observation system 312 comprises the same elements as those of the space observation system and additionally comprises:
.- at least one “remote or remote” ground station, 318, 320 for destination and reception of observation data, transmitted at a high speed by the at least one observation satellite 4, 6, .- a satellite communications geostationary 342, serving as a relay for retransmission of observation data between the at least one passing observation satellite (s) 4, 6 and the at least one destination and destination ground station (s) "remote (s) and remote (s)" reception 318, 320.
The destination, remote and remote ground stations 318, 320, are not optically visible from the relay platform 332 because of their distance from the local destination ground stations 12, 14, 16, from the aircraft overflight altitude and the roundness of the Earth, but are visible optically and radio-electrically from the geostationary satellite 342. These destination ground stations 318, 320, called “remote or remote”, and accessible directly from the geostationary satellite 342, form a second "remote" group of destination, remote or remote ground stations.
The destination ground stations 318, 320 include the same functions as the local destination ground stations 12, 14, 16, in particular the decryption with keys and associated indices which are specific to them.
It should be noted that, moreover, the security management, that is to say the loading of the keys and the transmission of the active key indices, is identical for all the stations 12, 14, 18, 318, 320.
Among the remote and remote destination ground stations 318, 320, at least one remote destination ground station, for example the ground station 320, can act as a diverting ground station, configured to receive telemetry data intended for a ground station local destination when the corresponding local link is unavailable, and to retransmit said telemetry data to a desired recipient.
The space observation system 312 differs from the space observation system 2 in that the relay platform 32 is replaced by a relay platform 332 having the same functions as said platform 32 and additional functions.
According to FIG. 7, the relay platform 332 is configured to serve as the first transmission relay at high speed of the spatial observation or telemetry data, between one or more non-geostationary traveling observation satellites, here the traveling satellites of observation 4 and 6, and at least one ground station of destination and reception of said data, here the destination ground stations 12, 14, 16, 318, 320, the transmission taking place in one or more predetermined visibility windows of the one or more scrolling observation satellites 4, 6 with respect to the aircraft 34.
The relay platform 332 includes a fifth transmit interface 362 and a fifth transmit antenna 364.
The fifth transmission interface 362 is configured to modulate the observation or telemetry data stored in the memory 106, and transmit, in a fifth optical or radiofrequency band, said modulated telemetry data, via the fifth transmission antenna 364 on a fifth uplink spatial wireless link 372 “of offset”, directly connecting the relay platform 332 to the geostationary satellite 342, said geostationary satellite 342 forming a second communication relay with respect to the telemetry data of the observation satellites 4, 6.
The communication relay platform 332 is configured to receive a switch command 376 of the encrypted data before sending to the ground, the command being developed and transmitted by the first control station 46.
In a nominal mode according to which the transmission on the second local downlink 128 allows the passage of a sufficient bit rate, the second interface 108 is activated and the telemetry observation data are routed by the memory 106 to said second interface 108 and local receiving stations.
In a regulation or emergency mode according to which the transmission on the second local downlink 128 does not allow the passage of a sufficient speed, after sending by the first control station 46 and reception by the relay platform 332 of an emergency mode switch command 376, the fifth interface 262 is activated and the telemetry observation data is routed by the memory 106 to said fifth interface 362 and the remote and remote reception stations 318, 320. The passage of the emergency mode in nominal mode is implemented by sending by the first control station 46 and reception by the relay platform 332 of a switch command 376 in nominal mode.
According to FIG. 8 and a first communication architecture 402 of the observation system 312 of FIG. 6, the communication system 402 of the observation system 312 uses a version 332-1 of the relay platform 332 which integrates to a degree enhanced the security functions for telemetry and remote control data from observation satellites 4, 6 like the relay platform 252 in FIG. 4.
In this architecture, the descent of secure telemetry from the observation satellites to the local destination stations 12, 14, 16 takes place nominally, below the relay platform 332-1 via double-level links, combining a choice of downlink of first level telemetry 122-1 or 122-2 and a downlink of second level telemetry taken from links 110-1, 110-2, and 110-3.
In emergency mode, the descent of encrypted telemetry from, for example the passing observation satellite 6, to the local destination ground station 12 takes place through the succession of encrypted links 122-2, 132, of a link 404 between the geostationary satellite 342 and the remote diversion ground station 20, a first repatriation link 406 between the remote diversion ground station 20 and the terrestrial control center 46, and a second repatriation link 408-2 between the terrestrial control center 46 and the destination ground station 12, the second level encryption of the telemetry being reported transparently at the level of the local destination ground station 12.
It should be noted that the standby mode via the geostationary satellite is applicable for non-visibility relay-station ground stations like ground stations 318, 320, but can also be applied to any station in visibility of the satellite without this choice being constrained by environmental conditions.
In nominal mode, the fall of secure telemetry from the observation satellites to the remote destination stations 318, 320 takes place via a double-level encryption link combining, as desired, a downlink of first-level telemetry 122-1 or 122-2 and a downlink of encrypted telemetry at the second level taken from a first compound link including the links 132 and 404 and a second compound link 414 including the link 132 and a second link between the geostationary satellite 42 and the destination ground station remote 18.
In this architecture, the rise of secure remote controls for observation satellites, from the terrestrial control center 46 to observation satellites 4, 6 takes place via the relay platform 332-1 through double-level links combining choice of the first uplink 152 of the first level and a connection 260-1 or 260-2 of the double uplink of second level remote controls.
According to FIG. 9 and a second communication architecture 432 of the observation system 312 of FIG. 6, the communication system 432 uses a version 332-2 of the relay platform 332 which only integrates the securing of the telemetry of the satellites of scrolling observation like the relay platform 202 in Figure 3 and serves only as a transparent relay vis-à-vis the securing of remote control data from observation satellites 4 and 6.
The second communications architecture 432 includes the same linkage and telemetry data protection elements as those of the first communications architecture 402.
The second communications architecture 432 differs from the first communications architecture 402 in that the rise of secure remote controls of the observation satellites, from the terrestrial control center 46 to the observation satellites 4, 6 takes place, first via the geostationary satellite through an uplink 452 between the terrestrial control center 46 and the geostationary satellite 342 and through a downlink 454 between the geostationary satellite 454 and the relay platform 332-2, then via the platform- relay 332-2 and through the uplink 260-1 or the uplink 260-2 to the corresponding observation satellite 4 or 6.
The remote control observation satellite data is encrypted at the first terrestrial control center 46 and this data encryption is reported transparently via the geostationary satellite 342 and the relay platform 332-2 at the observation satellites. 4 and 6.
According to FIG. 10 and a third communications architecture 462 of the observation system 312 of FIG. 6, the communications system 462 uses a version 332-3 of the relay platform 332 which only integrates the securing of the telemetry of the satellites of moving observations, like the relay platform 202 in Figure 3, and which does not participate in the transmission of remote control data from the first terrestrial control center 46 or from the second satellite control center 48 to the satellites scrolling observation 4, 6.
The third communications architecture 462 differs from the first and second communications architectures 402, 432 in that the rise of secure remote controls for observation satellites 4, 6, from the first terrestrial control center 46 or from the second satellite control center 48 to the observation satellites 4, 6 takes place directly, via a dedicated spatial uplink of remote controls 4801 or 480-2, between the terrestrial control center 46 and the corresponding observation satellite 4 or 6.
In general, the implementation of a method for protecting the data from observation telemetry and from the remote controls of observation satellites by the observation system of FIG. 1 using the platform of FIG. 6 comprises a loading step. sets of encryption / decryption keys executed during a key initialization or key renewal phase, and a step of transmitting the indices of the active keys.
The double level of encryption, between the observation satellites and the relay platform on the one hand, and between the relay platform and the destination ground stations makes it possible to implement either:
.- a mix or redistribution of telemetry data between observation satellites and destination ground stations, all combinations being a priori possible, each individual link being specifically encrypted.
.- on-board management of the allocation of uplink data (mission plans) to the various observation satellites, which has the effect of reducing the complexity of ground-to-platform 20 relay transmissions and their securing. management on board of the relay platform of the allocation of downlink telemetry data from the observation satellites to the various reception terminals on the ground, via a matrix allocation of these data, all or part of the data from a satellite j which can be transmitted to a destination ground station k. This allows a total modularity of broadcasting telemetry data, combined with securing this broadcasting.

权利要求:
Claims (14)
[1" id="c-fr-0001]
CLAIMS .1 Communications relay platform of a space observation system, configured to be carried on board an aircraft (34) flying above the clouds, and configured to serve as a high altitude relay for transmission at a rate high of spatial observation data, called telemetry, between at least one non-geostationary observing satellite (4,6) parading and at least one destination ground station (12, 14, 16) and of reception of said data, the transmission from the observation satellite (s) to the high altitude relay which can take place in one or more predetermined visibility windows of the observation satellite (s) (4, 6) parading with respect to the aircraft (34), and the data transmission from the aircraft to the ground can take place permanently, the relay platform comprising a first receiving antenna (102), configured to receive in a first band o ptic or radiofrequency of the observation data, transmitted over a first downlink wireless spatial link (122), connecting at least one traveling observation satellite to the relay platform, and a first reception interface (104), connected to the first reception antenna (102) and configured to demodulate the data received by the first antenna and save it in a memory (106), and a second transmission interface (108), configured to modulate the observation data stored in the memory (106), and transmit in a second radiofrequency band said modulated data via a second transmit antenna (110) on a second downlink wireless aerial link (128) directly connecting the relay platform to at least one destination ground station (12, 14, 16), and the relay platform being characterized in that it comprises a first decryption / encryption chain with double descenda level nt (204) telemetry data retrieved from at least one passing observation satellite (s) (4, 6) to the destination ground station (s) (12, 14, 16).
[2" id="c-fr-0002]
2. communications relay platform according to claim 1, in which the first frequency band of the first downlink wireless spatial link (122) is an optical or radiofrequency band, and / or
The second frequency band of the second downlink (128) is an optical or radio frequency band.
[3" id="c-fr-0003]
3. Communications relay platform according to any one of claims 1 to 2, further comprising a third reception interface (142), configured to demodulate secure remote control data of the relay platform and / or the satellite (s) (s) parading observation (s), developed and transmitted on a third link (152) dedicated by a ground control center (46) of the space observation system.
[4" id="c-fr-0004]
4. Communications relay platform according to any one of claims 1 to 3, in which the first decryption / encryption chain with double descending level (204) is configured:
for each passing observation satellite (4, 6) and the corresponding received telemetry data, decrypting at a first descending level said telemetry data, encrypted and transmitted by said traveling observation satellite on the first downward space link (122) and demodulated by the first interface (104), using active keys for decrypting the data of the descending first level telemetry data, associated with said traveling satellite and with indices of active keys for encryption / decryption of the first telemetry data. descending level, said active encryption / decryption key indices being transmitted jointly with said encrypted telemetry data and being associated in a unique manner with said moving observation satellite and with said first descending active decryption keys; then .- for each destination ground station (12, 14, 16) and the corresponding data intended for them of telemetry, decrypted at the first descending level and coming from one or more observation satellites (4, 6), encrypt at a second descending level the telemetry data decrypted at the first descending level using an active key for encrypting the descending second level telemetry data, associated with said destination ground station, and adding to said encrypted second level descending data an index active key for encryption / decryption of second descending level telemetry data, uniquely associated with said destination ground station and said active key for second down level encryption.
[5" id="c-fr-0005]
5. A communications relay platform according to claim 4, in which the first decryption / encryption chain with double descending level (204) of telemetry data, retrieved from the passing satellite (s) (4, 6) ) towards the destination ground station (s), comprises a first module (212) for managing the encryption / decryption keys of the double downlink level, a second module (214) for decryption at a first downlink level of the data of telemetry, transmitted over the first downlink space link (122) and demodulated by the first interface (104), and a third encryption module (216) at a second downlink level of decrypted telemetry data at the first downlink level; and the first module (212) for managing the descending double level encryption / decryption keys of telemetry data is configured to initially receive a first set of one or more sets of descending first level telemetry decryption keys ; and .- initially receive a second set of one or more sets of encryption keys for telemetry data of second descending level; and each set of telemetry decryption keys relating to the first downlink level is associated with a moving observation satellite, and each telemetry decryption key relating to the first downlink level of each set is matched to and uniquely identified by a first descending level encryption / decryption key index; and each set of telemetry data encryption keys relating to the second downlink level is associated with a destination self station, and each telemetry data encryption key relating to the second downlink level of each set is matched and uniquely identified by a key index of encryption / decryption at the second descending level.
[6" id="c-fr-0006]
6. Communications relay platform according to claim 5, in which the first module (212) for managing encryption / decryption keys with double level descending telemetry data is configured to execute, on reception via the third remote control interface. dedicated, secure and sent by the terrestrial control center, modifications of part or all of the decryption keys of the telemetry data at the first down level and / or the encryption keys of telemetry data at the second down level.
[7" id="c-fr-0007]
7. Communications relay platform according to any one of claims 4 to 6, in which the first reception antenna (102), the first reception interface (104), and the memory (106) are configured to receive, demodulate. and separately save telemetry data, encrypted at the first downlink level and transmitted by at least two non-geostationary moving observation satellites on the first downward space link (122), and / or the second transmit antenna (110), the second transmit interface (108), are configured to separately modulate and transmit encrypted telemetry data at the second downlink level to at least one destination ground station on the second downlink wireless air link (128); and the first descending double-level decryption / encryption chain (204) of telemetry data, repatriated from the passing satellite (s) (4, 6) to the destination ground station (s) ( 12, 14, 16), comprises a matrix allocator (224) for decrypted telemetry received from the same passing observation satellite, at different destination ground stations, according to an allocation table (226) loaded by remote controls, l matrix allocator (224) being connected in series between the second decryption module (214) and the third encryption module (216).
[8" id="c-fr-0008]
8. communications relay platform according to any one of claims 1 to 7, further comprising a second decryption / encryption chain with double rising level (254) of the remote control data of the satellite (s) running (s) observation received via the third reception interface (142) of the third dedicated link of secure remote controls (152) coming from the terrestrial control center (46).
[9" id="c-fr-0009]
9. A communications relay platform according to claim 8, in which the second decryption / encryption chain at double rising level (254) of the remote control data of the scrolling observation satellite (s) (4, 6) ) is configured:
.- for each destination scrolling observation satellite (4, 6) and the remote control data of said corresponding satellite, decrypt at a first level the remote control data transmitted by the terrestrial control center (46) on the third link (152) and demodulated by the third interface (142), using an active key for decrypting first level remote control data, associated with said observation satellite and with an active key index for encryption / decryption of data from first level remote control upstream, said active key index encryption / decryption of the remote control data being transmitted jointly with the remote control data encrypted by the terrestrial control center (46) and being associated in a unique manner with the traveling satellite and with said first level up decryption key; then .- for each destination scrolling observation satellite (4, 6) and the decrypted remote control data intended for it, encrypt at a second level rising the decrypted remote control data at the first level rising using an active key of d encryption of the second uplink level remote control data, the active key of encryption of the second uplink level remote control data being associated with the destination observation satellite, and adding to said second uplink level remote control data, a key index active encryption / decryption of remote controls, uniquely associated with said observation satellite and with said active encryption key of second uplink level.
[10" id="c-fr-0010]
10. Communications relay platform according to claim 9, further comprising a fourth transmission interface (256), configured to modulate remote control data from at least one moving observation satellite (4, 6), and transmit said modulated remote control data via a fourth transmitting antenna (258) on a fourth uplink spatial wireless link (260) directly connecting the relay platform to the (x) moving observation satellite (s) (4, 6);
and in which the second ascending double level decryption / encryption chain (254) of the remote control data of the observing satellite (s) comprises a fourth module (262) for managing the encryption keys / decryption of the double rising level, a fifth module (264) of decryption at a first rising level of the remote control data, transmitted on the third link (152) and demodulated by the third interface (142), and a sixth module (266) of encryption at a second uplink level of the remote control data decrypted at the first uplink level; and the fourth module (262) for managing the encryption / decryption keys at double level amount of the remote controls of the traveling satellite (s) is further configured to initially receive a third set of one or more sets of decryption keys for first level remote controls, .- initially receiving a fourth set of one or more sets of encryption keys for second level remote controls; and each set of remote control decryption keys for the first uplink level is associated with a scrolling observation satellite, and each remote control decryption key data for the first uplink level of each set is matched to and uniquely identified by a index key for encryption / decryption of remote control data at the first uplink level; and each set of remote control encryption keys for the second uplink level is associated with a scrolling destination observation satellite, each remote control encryption key for the second uplink level of each set is matched to and identified so unique by an encryption / decryption key index at the second rising level.
[11" id="c-fr-0011]
11. A communications relay platform according to claim 10, in which the fourth module (262) for managing the encryption / decryption keys at two levels of the remote control data of the traveling satellite (s) is configured for execute, on reception via the third interface (142) of dedicated remote controls, secured and sent by the terrestrial control center (46), modifications of part or all of the decryption keys of the remote control data at the first uplink level and / or remote control data encryption keys at the second uplink level.
[12" id="c-fr-0012]
12. communications relay platform according to claim 1, further comprising a fifth transmission interface (362), configured to modulate the observation data stored in the memory (106), and transmit in a fifth optical or radio frequency band, said data modulated via a fifth transmitting antenna (364) on a fifth uplink spatial wireless link (372) directly connecting the relay platform to a geostationary satellite (342), the memory (106) being configured to route, in a piloted manner from the ground by sending a dedicated command (376), the telemetry data on the fifth transmission interface (362), instead of the second transmission interface (108) taken as destination port in nominal mode.
[13" id="c-fr-0013]
13. Space system comprising at least one non-geostationary observing satellite (s) (4, 6) (4, 6), at least one destination ground station (s) (12, 14, 16) and for receiving observation data transmitted at a high rate by the at least one observation satellite (4, 6), an aircraft (34) operating at a high altitude exceeding that of the clouds, and a platform- communications relay (32) on board the aircraft (34) and serving as a relay for transmission of observation data or telemetry between the at least one observation satellite (4, 6) and the at least two destination (12, 14, 16) and data reception ground stations, in which the communications relay platform (32; 332) is defined according to any one of claims 1 to 12, and the aircraft (34) is included in the set formed by drones, stratospheric airships or airplanes.
[14" id="c-fr-0014]
14. The space system as claimed in claim 13, further comprising a geostationary satellite (342) and at least one remote and remote ground station (320), connected to said geostationary satellite (342) by a downward geostationary space link, and in which the relay platform (332) comprises a fifth transmission interface (362), configured to modulate the observation data stored in the memory (106), and transmit in a fifth optical or radiofrequency band said modulated data via a fifth antenna d transmission (364) on a fifth uplink space wireless link (372) directly connecting the relay platform to a geostationary satellite (342), the memory (106) being configured to route, in a piloted manner from the ground by sending a dedicated command (376), the telemetry data on the fifth transmission interface (362) instead of the second transmission interface (108) pr ise as destination port in nominal mode.
1/10
CD

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CN112398506A|2019-01-31|2021-02-23|上海微小卫星工程中心|Satellite-ground/relay integrated measurement and control system|

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FR3105673A1|2019-12-20|2021-06-25|Thales|OPTICAL OPTICAL SPACE DATA TRANSMISSION SYSTEM FSO IN THE INFRARED WAVELENGTH DOMAIN|

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CN111698021A|2020-04-30|2020-09-22|彩虹无人机科技有限公司|Ku and Ka dual-frequency satellite communication link equipment|

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CN112803991B|2021-03-16|2021-10-15|中国人民解放军32039部队|Target range measurement and control system and method|

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CN112994784B|2021-04-26|2021-09-17|北京航天驭星科技有限公司|Method for receiving satellite telemetering data and method for sending instruction to satellite|

法律状态:
2017-11-27| PLFP| Fee payment|Year of fee payment: 2 |

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2018-06-15| PLSC| Search report ready|Effective date: 20180615 |

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2019-11-28| PLFP| Fee payment|Year of fee payment: 4 |

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2020-11-25| PLFP| Fee payment|Year of fee payment: 5 |

优先权:

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申请号 | 申请日 | 专利标题

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FR1601749|2016-12-08|

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FR1601749A|FR3060246B1|2016-12-08|2016-12-08|TELEMEURING DATA COMMUNICATION RELAY PLATFORM FROM ONE OR MORE SATELLITE SATELLITEOF OBSERVATION TILTINGTO THE GROUND|FR1601749A| FR3060246B1|2016-12-08|2016-12-08|TELEMEURING DATA COMMUNICATION RELAY PLATFORM FROM ONE OR MORE SATELLITE SATELLITEOF OBSERVATION TILTINGTO THE GROUND|

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US16/467,959| US10707950B2|2016-12-08|2017-10-12|Relay platform for communicating telemetry data from one or more moving observation satellite to the ground|

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CA3046412A| CA3046412A1|2016-12-08|2017-10-12|Plateforme-relais de communication de donnees de telemesures depuis un ou plusieurs satellite d'observation defilant vers le sol|

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EP17781503.2A| EP3552323B1|2016-12-08|2017-10-12|Relay platform for communicating telemetry data from one or more moving observation satellite to the ground|

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PCT/EP2017/076065| WO2018103926A1|2016-12-08|2017-10-12|Relay platform for communicating telemetry data from one or more moving observation satellite to the ground|

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JP2019530727A| JP2020501452A|2016-12-08|2017-10-12|Relay platform for communicating telemetry data from one or more mobile observation satellites to the ground|

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ES17781503T| ES2829576T3|2016-12-08|2017-10-12|Relay platform for communicating telemetry data from one or more roaming observing satellites to ground|