• 专利附录
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    • 专利摘要:
    The invention relates to a method (100) for simulating the estimation of a delay of realization of satellite images associated with at least one predetermined zone of the Earth (20), by at least one Earth observation satellite comprising an optical imaging system, the predetermined area being pre-divided (110) according to a mesh grid (11), the acquisition being scheduled to be triggered from a start date of analysis, the method comprising the steps consisting of: (a) conducting a census (120) of the meshes scheduled to be overflown by the satellite at a current iteration date, from the orbital characteristics of the satellite at the current iteration date, so as to obtain meshes candidates, (b) identify (130) among the candidate meshes, from a satellite mission plan, those for which a plan for the acquisition of at least one satellite image is provided, so as to obtain planing meshes, (c) obtaining (140) at least a first cloudiness value for each of the planned meshes, (d) identifying (140) among the planned meshes, those for which the first associated cloudiness value is beyond a predetermined validation threshold value, so as to obtain validated meshes, (e) repeating the steps (a) to (d), one or more times until each of the meshes of said grid is included in the meshes validated, taking into consideration at each iteration the unidentified meshes as validated and a following period of the current iteration date considered in the previous iteration, (f) determining (150) the delay of realization of satellite images to from the number of iterations made in step (e).
    公开号:FR3069651A1
    申请号:FR1757161
    申请日:2017-07-27
    公开日:2019-02-01
    发明作者:Cecilia Amselem；Eric Villemejeanne；Jean-Christophe Angulo
    申请人:Centre National dEtudes Spatiales CNES；Airbus Defence and Space SAS；
    IPC主号:
    专利说明:

    Title: Device and method for simulating the estimation of a timeframe for producing satellite images of the Earth
    Description
    Technical Field [001] The present invention relates to the field of satellite remote sensing. More specifically, it relates to a device and a method for simulating the estimation of a delay in producing satellite images of the Earth by optical acquisition techniques.
    PRIOR ART [002] The circumterrestrial space contains a number of Earth observation satellites making it possible in particular to monitor parameters of the Earth system (oceans, atmospheres, natural resources, impacts of human activities, etc.), obtain maps or provide information enabling the defense of States. To do this, these systems are based on a set of satellite imagery data, that is to say a set of measurements carried out using on-board instruments at satellite level.
    Due to the trivialization of Earth observation, requests for satellite imagery are increasing day by day. Some of the satellite’s resources are limited, such as the number of shots that can be taken while flying over an area of the globe or the capacity to transmit data to the ground. It is therefore necessary to plan for the long term the use of these resources while meeting the demands for satellite imagery.
    One of the elements for developing such a schedule is the time required to complete a request for satellite imagery (in English, timeto-acquire). Such a delay corresponds to the time elapsed between the activation of a satellite imagery request and the delivery of the imagery results to the client. In the field of optical Earth observation, satellite imagery is dependent on weather conditions. Indeed, clouds present in the acquisition zone can hide the object or the territory that we are trying to observe. However, it is well known that long-term weather forecasts have a lot of uncertainty, which makes it difficult to determine the lead time for a particular satellite imagery request. Thus, in practice, it is common to estimate the lead time based primarily on the experience of the operator of the Earth observation system as well as his knowledge of the climatology of the area to be acquired.
    The subjective nature of this estimate is difficult to reconcile with the ever-increasing demands for reliability and precision required by customers in satellite remote sensing systems.
    -2Summary of the invention [006] The present invention therefore aims to overcome such drawbacks by providing a method and a device for estimating the time required to satisfy a request for satellite imagery associated with a predetermined area of the Earth, by at least one Earth observation satellite comprising an optical imaging system.
    The invention relates to a method for simulating the estimation of a delay in producing satellite images associated with at least one predetermined area of the Earth, by at least one Earth observation satellite comprising a optical imaging system, the predetermined area being previously divided according to a mesh grid, the acquisition being scheduled to be triggered from a start date of analysis. The process is remarkable in that it includes the steps of:
    (a) selecting a plurality of grid cells, intended to be overflown by the satellite on a current iteration date, from the orbital characteristics of the satellite on the current iteration date, so as to obtain candidate cells, the current date of iteration corresponding to a date around the date of start of analysis in a year prior to the year associated with the date of start of analysis, (b) identify among the candidate meshes, starting from a mission plan of the satellite, those for which a planning of acquisition of at least one satellite image is planned, so as to obtain planned meshes, (c) obtaining at least a first value of cloudiness for each of the meshes planned, the first cloud value corresponding to a weather observation and / or forecast, respectively observed on the current date of iteration or carried out for the current iteration date, (d) identify among the planned meshes, those for which the first associated cloud value is beyond a predetermined validation threshold value, so as to obtain validated meshes, (e) repeat steps (a) to (d), one or more times until each of the meshes of said grid is included in the validated meshes, taking into account at each iteration the meshes not identified as validated and a following period from the current iteration date considered in the previous iteration, (f) determine the timeframe for producing satellite images from the number of iterations carried out in step (e).
    [008] Preferably, step (a) further comprises the steps consisting in:
    - obtain at least a second cloud value for each of the candidate cells, the second cloud value corresponding to a meteorological observation and / or a meteorological forecast, respectively observed on the current date of iteration or carried out on the current date of iteration , and,
    - identify among the candidate cells, those for which the second associated cloudiness value is beyond a predetermined selection threshold value different from the predetermined validation threshold value.
    The predetermined selection threshold value and the predetermined validation threshold value may preferably correspond to a threshold value of percentage of clear sky. Preferably, the validation threshold value is greater than the selection threshold value.
    [0010] Preferably, step (f) further comprises the step consisting in determining at least one statistical quantity and / or at least one posterior probability from a plurality of determined time frames for producing satellite images. in step (d).
    The invention also relates to a computer program product, which, when executed by a computer, is arranged to execute a method according to the invention; the computer program being, optionally, stored on a computer-readable medium.
    The invention also aims a device for simulating the estimation of a delay in producing satellite images associated with at least one predetermined area of the Earth, by at least one Earth observation satellite comprising an optical imaging system, the predetermined area being previously divided according to a mesh grid, the acquisition being scheduled to be triggered from a start date of analysis, the device comprising:
    - a memory configured to store:
    - the mesh grid associated with the predetermined area,
    - the orbital characteristics of the satellite at a current iteration date, the current iteration date corresponding to a date around the start date of analysis in a year prior to the year associated with the start date analysis, and
    - at least a first cloud value for each of the grid cells, the first cloud value corresponding to an observation and / or a weather forecast, respectively observed on the current date of iteration or carried out for the current date of iteration ,
    a processor coupled to the memory and configured to select a plurality of meshes of the grid, intended to be overflown by the satellite on the current date of iteration from the orbital characteristics of the satellite on the current date of iteration, so to obtain candidate meshes, the processor being further configured to:
    (a) identify among the candidate meshes, from a satellite mission plan, those for which a planning of acquisition of at least one satellite image is planned, (b) identify among the candidate meshes, those for which the first associated cloudiness value is beyond a predetermined validation threshold value, so as to obtain planned meshes, (c) repeat operations (a) and (b), one or more times until each meshes of said grid is included in the validated meshes, taking into consideration at each iteration the meshes not identified as validated and a period
    -4 following the current iteration date considered in the previous iteration, (d) determine the timeframe for producing satellite images from the number of iterations carried out during the operation (c).
    Preferably, the memory is further configured to store a second cloud value for each of the candidate cells, the second cloud value corresponding to a meteorological observation and / or a meteorological forecast, respectively observed on the current date of iteration or carried out for the current date of iteration, and, the processor is further configured to identify among the candidate meshes, those for which the second associated cloudiness value is beyond a predetermined selection threshold value different from the predetermined validation threshold value, so as to obtain the candidate meshes.
    The predetermined selection threshold value and the predetermined validation threshold value may preferably correspond to a threshold value of percentage of clear sky. Preferably, the validation threshold value is greater than the selection threshold value.
    Preferably, the processor is further configured to determine, during operation (d), at least one statistical quantity and / or at least a posterior probability from a plurality of completion times d 'satellite images determined during operation (c).
    Brief description of the drawings Other characteristics and advantages of the invention will be better understood on reading the description which follows and with reference to the accompanying drawings, given by way of illustration and in no way limiting.
    Figure 1 shows a flowchart according to the invention.
    Figure 2 shows a mesh grid surrounding a portion of the Earth.
    Figure 3 shows a schematic functional view of an estimation device according to an implementation of the invention.
    Figures 4a, 4b, 4c, 4d and 4e show an example of implementation according to the invention.
    FIG. 5 represents a distribution of the simulated completion time for several years for an example of request for satellite imagery.
    For reasons of clarity, the elements shown are not to scale with respect to each other, unless otherwise stated.
    Description of the embodiments In the context of the description, the term “Earth observation system” means a system comprising satellite constellations such as Landsat, Spot or even Pleiades. In addition, it is specified that the invention relates to optical satellite systems, for which the acquisition of images of the Earth is dependent on an illumination.
    -5 [0025] [0027] [0028] [0028] solar reflected by the ground. These systems use passive sensors to record the solar radiation reflected from the ground, in various wavelengths.
    The general principle of the invention is based on the observation that long-term weather forecasts are not very reliable. It is therefore not advisable to base oneself on these latter to estimate the time necessary for the realization of satellite images associated with a predetermined area of the Earth. Thus, according to the invention, it is proposed to carry out one or more simulations of the process of acquiring satellite images associated with a predetermined area of the Earth. The process of acquiring images covering the period from the activation of a request for satellite imagery requested by a client until the provision of imagery results to this same client. In the invention, it is a matter of carrying out each simulation from observations and / or past weather forecasts. In this way, it is possible to determine the time that it would have taken to the Earth observation system to take satellite images of the predetermined area of the Earth during the past period concerned. This amount of time determined according to the past can then be used as a basis for estimating the future timeframe for producing satellite images.
    FIG. 1 illustrates a method 100 functionally describing the general principle of the simulator according to the invention.
    In the example of FIG. 1, we consider that we receive a request for satellite imagery Rq similar to the requests that are received and processed in mission centers for satellites. However, it is also envisaged that we receive several concurrent Rq requests. An Rq request is scheduled to be triggered / activated from an analysis start date. By date, we mean the day, the month and the year.
    The request Rq defines at least one predetermined area of the Earth in which the acquisition in satellite imagery must be carried out. In one example, the predetermined area of the Earth is defined by one or more polygons whose vertices correspond to geographic positions of the terrestrial globe. In a particular implementation, the request Rq is intended to be associated with a predetermined Earth observation system which is configured to fly over the predetermined area of the Earth.
    Subsequently, in step 110, known as the mesh step, the predetermined area of the Earth is divided according to a grid composed of meshes in order to obtain the required meshes Md. The grid means, for example, a horizontal and vertical grid. By mesh is meant any one of the elementary quadrilaterals that make up the grid. For example, each mesh in the grid has a square shape or is close to a square, for example, a rectangular shape. FIG. 2 illustrates an example of a mesh grid 10 superimposed on a portion of the Earth. In a first example, the grid according to the invention is in the form of an image file in which each mesh associated with the predetermined area is geo-referenced. In a second example, the grid according to the invention is presented under the
    -6form of a text file in which each line describes at least one mesh of the grid with geo-referencing information associated with the predetermined area.
    In a step 120, called a census, so-called candidate meshes Mc are determined from among the requested meshes Md. For this, use is made, at a current iteration date, of the orbital characteristics of at least one satellite. observation configured to fly over the predetermined area of the Earth, to determine from the requested meshes Md, those which would be overflown by the observation satellite on the current date of iteration.
    The term orbital characteristics of a satellite is understood to mean conventional characteristics such as altitude, number of orbits per day or inclination of the orbit. Other parameters of the system can also be defined in conjunction with the orbital characteristics of a satellite, such as the list of ground stations allowing the descent of the images produced by the satellite, the resolution of the imaging system, the spectral bands supported by the system. imagery from the satellite, the swath of the optical instrument or the limits of angle of incidence authorized for taking pictures.
    By current iteration date is meant a date taken into account during an iteration of a simulation of the time taken to complete the request Rq. The current iteration date is located around the start date in a year prior to the year associated with the start date of the Rq request. The term “previous year” is understood to mean a year preceding the year associated with the date on which analysis of the query Rq begins. For example, it can be two, five, eight, twelve, twenty or even thirty years before the year associated with the start date of the Rq request. During a simulation according to the invention, the current iteration date is initialized to a date of initialization of the simulation. The start date of the simulation is determined from the start date of analysis of the Rq request. In an example, we can consider that the starting date of analysis of the request Rq is planned for the dd / mm / YYYY where dd corresponds to the day, mm to the month and YYYY the year concerned. In this example, we can also consider that the previous year to take into account is five years before the year associated with the date on which the analysis of the query Rq begins. In this case, the initialization date of the simulation considered corresponds to the date of dd / mm / (YYYY-5). Then, during a simulation, the current iteration date is incremented according to at least one predetermined criterion. In an alternative to the example, several simulations are carried out, each simulation relating to a given previous year. In this case, if eight simulations are carried out over the last eight years preceding the start date of analysis of the query Rq, then the date of initialization of each simulation will correspond respectively to the dates of dd / mm / (YWY -1), dd / mm / (YYYY-2), dd / mm / (YYYY-3), dd / mm / (YYYY-4), dd / mm / (YYYY-5), dd / mm / (YYYY -6), dd / mm / (YYYY-7) and dd / mm / (YYYY-8).
    -7 In a first particular implementation of step 120, only the requested meshes Md which are scheduled to be overflown by day, can be considered as candidate meshes Mc.
    In a second particular implementation of step 120, only the requested meshes 5 Md which are intended to be overflown while being little or not masked by clouds, can be considered as candidate meshes Mc. For that, one associates with each requested mesh Md a first value of cloudiness Vn1. Thus, only the requested meshes Md which are intended to be overflown and whose first cloud value is above a selection threshold value, can be considered as candidate meshes Mc.
    In one example, the predetermined selection threshold value is a cloud threshold as a threshold value of percentage of clear sky.
    Conventionally, the term “cloudiness” is understood to mean the part of the sky covered by all or part of the clouds at the level of each mesh of the grid 10. It may be, for example, a data file ERA- Interim produced by CEPMMT (European Center for
    Medium-Term Weather Forecast, or ECMWF in English for European Center for Medium-Range Weather Forecasts). Such a file, according to the invention, can include a cloud value for each of the requested meshes Md, and this, on one or more dates within one or more years preceding the year associated with the start date. analysis.
    In a first implementation, the first cloud value corresponds to a meteorological observation observed on the current date of iteration. In an example of the first implementation, the meteorological observation is carried out during a year prior to the year associated with the date of commencement of analysis, the month 25 having the same name and the day having the same date as the month and day of the start date.
    In a second implementation, the first cloud value corresponds to a weather forecast made for the current date of iteration. In an example of the second implementation, the forecast was made for the same date as the predefined start date in at least one year prior to the year associated with the start date of analysis.
    In an example of the second particular implementation of step 120, the candidate meshes Mc are prioritized according to at least one predetermined priority criterion. For example, a higher priority can be given to candidate meshes Mc whose first cloud value Vn1 is low. In another example, one can prioritize the candidate meshes Mc according to a predetermined priority value. The predetermined priority value can be determined in the request Rq or in step 110. It will be noted that it is also envisaged to use several predetermined priority criteria in combination or independently.
    -8 In a step 130, called calculation of the mission plan, so-called planned meshes Mp are determined from among the candidate meshes Mc. For this, we simulate, on the current iteration date, the generation of a mission plan of the observation satellite considered from candidate meshes Mc and from the request Rq. Thus, only the candidate meshes Mc which are planned to be acquired by the satellite considered, can be considered as planned meshes Mp. By mission plan (in English, mission plan) is meant the programming plan of the satellite in question which is downloaded / sent to the satellite via the control center and which makes it possible to take pictures of the predetermined area of the Earth according to an order and shooting characteristics provided in the plan. For example, the priority associated with each candidate mesh Mc can be taken into consideration when developing the mission plan. It is known that the mission plan takes into account the kinematic constraints linked to the platform and also integrates the emptying plans on the various reception stations. Such a mission plan can be obtained by a mission plan generator of known type, for example, as described in application FR3039728. In the invention, it is intended to take into account the satellite load (in English, satellite load) in establishing the mission plan. By satellite load is meant a plurality of requests Rq processed concurrently by the satellite at a given time. As part of a simulation, we can consider the current and / or future load of the Earth observation satellite concerned.
    In a step 140, called validation, we simulate the validation of the images acquired once downloaded to the ground. For this, we determine, on the current iteration date, so-called validated meshes Mv among the planned meshes Mp. In practice, only the planned meshes Mp which have not been masked by clouds, can be considered as meshes validated Mv. For that, one associates with each planned mesh Mp, a second value of nebulosity Vn2. Thus, only the planned meshes Mp whose second cloud value is above a threshold validation value, can be considered as validated meshes Mv. In one example, the predetermined validation threshold value is a threshold percentage of clear sky. For example, a threshold value of percentage of clear sky between 50% and 100% can be envisaged, more preferably between 60% and 90%. In a particular implementation, the predetermined validation threshold value is greater than the predetermined selection threshold value.
    The invalidated MiV meshes in step 140 are reintroduced into an iteration loop formed by steps 120, 130 and 140, until each of the requested meshes Md is included in the set of validated meshes Mv . For this, at each iteration of the simulation, we take into account a following period of the current iteration date considered in the previous iteration. In an example, the next period of the current iteration date considered in the previous iteration corresponds to the next day of the current iteration date considered in the previous iteration. However, other periods can be envisaged such as for example, a predetermined period
    -9 [0044] [0044] [0045] [0046] [0047] [0048] to the next satellite orbit, one or more days, weeks, months or any other suitable duration.
    Finally, in a step 150, for a simulation that has reached completion after one or more iterations, the delay Dr necessary for the production of satellite images is determined from the number of iterations performed during the simulation. In one example, this is, at least, the period of time between the date of initialization of the simulation in question until the date of completion of the simulation in question. In this example, other operational periods Po can also be added, such as the period necessary for the preparation and delivery of the imaging results to the client. This may in particular include image processing operations according to the wishes of the client.
    The example of FIG. 3 illustrates a particular implementation of the method 100 of FIG. 1. FIG. 3 shows a device 200 for simulating the estimation of the time taken to produce satellite images associated with a predetermined area of the Earth. The device 200 includes a processor 210 and a memory 220 which are mutually coupled.
    The memory 220 is configured to store a grid associated with the predetermined area of the Earth defined in the request Rq. In a particular implementation, the memory 220 is configured to store a plurality of grids, each being associated with a predetermined area of the Earth defined in the request Rq. In another particular implementation, the memory 220 is configured to store a grid associated with a plurality of predetermined areas of the Earth defined in the request Rq. In addition, the memory 220 is also configured to store the orbital characteristics of at least one observation satellite configured to fly over the predetermined area of the Earth, at least on the current date of iteration of the simulation. Finally, the memory 220 is configured to store the first cloud value Vn1 and the second cloud value Vn2 for each of the requested cells Md.
    The processor 210 is configured to implement steps 110, 120, 130, 140 and 150 of the method 100 according to the meteorological data available. In general, the invention is intended to use a meteorological observation observed on the current date of iteration and / or a meteorological forecast produced for the current date of iteration
    In a first implementation, only past weather forecasts are available. In this case, the processor 210 is configured to use the weather forecasts passed in step 120.
    In a second implementation, only past weather observations are available. In this case, the processor 210 is either configured to use the weather observations passed in steps 120, and 140, or to use the weather observations passed in step 140.
    In a third implementation, we have observations and past weather forecasts. In this case, the processor 210 is configured to use the
    - 10 [0050] [0051] [0052] [0053] [0054] weather forecasts passed in step 120 and use the weather observations in step 140.
    In order to better understand the operation of the device 200, let us consider the example of a simulation in connection with FIGS. 4a, 4b, 4c, 4d and 4e. In this example, the processor 210 is configured according to the second alternative of the second implementation, as described above. In practice, only past meteorological observations are available which are used by the processor 210 in the implementation of step 140.
    First, it is assumed that we receive, at a mission center for satellite, a file comprising a request for satellite imagery Rq associated with a predetermined area of the Earth. FIG. 4a, in connection with FIG. 3 presented above, illustrates a predetermined area 20 defined by the request Rq. Then, we also assume that the start date of analysis of the request Rq is scheduled for dd / mm / YYYY where dd corresponds to the day, mm to the month and YYYY the year concerned. It is also assumed that the memory 220 stores the orbital characteristics of at least one observation satellite configured to fly over the predetermined area of the Earth 20, and this, at each current date of iteration of the simulation. Finally, it is assumed that the memory 220 stores a second cloud value Vn2 for each mesh requested Md by the request Rq. We also consider in the example that the second cloud value Vn2 was observed on the date of dd / mm / (YYYY - T) where T corresponds to an integer. In the example, we consider that T takes the value 10, so that the memory 220 stores at least a second value of cloudiness Vn2 observed ten years before the date of commencement of analysis of the dd / mm / YYYY, it is i.e. on the date of dd / mm / (YYYY-10). Thus, the simulation initialization date is dd / mm / (YYYY-10).
    In operation, the processor 210 first implements step 110 in order to obtain the requested meshes Md. FIG. 4b delimits by a bold line 11 all of the requested meshes Md which result from the cutting of the predetermined area 20.
    Subsequently, as indicated above, the processor 210 implements step 120 in order to obtain the candidate meshes Mc. It is then a question of identifying among the requested meshes Md, those which would be overflown by the observation satellite on the current date of iteration.
    Then, the processor 210 implements step 130 in order to obtain the planned meshes Mp. It is then a question of obtaining the meshes of the grid 11 which are intended to be acquired by the observation satellite on the date of dd / mm / (YYYY-10).
    Subsequently, the processor 210 implements step 140 in order to obtain the validated meshes Mv. It is then a question of identifying among the planned meshes those for which the second cloud value Vn2 is beyond a predetermined validation threshold value. FIG. 4c illustrates by hatching the meshes of grid 11 which would have been validated on the date of dd / mm / (YYYY-10).
    - 11 According to FIG. 4c, only part of the meshes of grid 11 would have been validated on the date of dd / mm / (YYYY - 10), so that processor 210 needs to continue the simulation from meshes invalidated Miv during the implementation of step 140 by the processor 210. For this, the processor 210 implements an iteration loop of the 5 steps 120, 130, 140, 150.
    However, in the invention, during the execution of a subsequent iteration of the simulation, the processor 210 is configured to take into account the following period of the current iteration date considered in the previous iteration.
    In the example of FIG. 4, the processor 210 takes into account the next day of 10 the current date of iteration considered in the previous iteration. Thus, during the second iteration, the processor 210 selects on the date of (dd + 1) / mm / (YYYY-10), the planned meshes Mp from the invalidated meshes Miv. Then, the processor 210 identifies among the planned meshes Mp those for which the second associated cloud value, on the date of (dd + 1) / mm / (YYYY - 10), is beyond the validation threshold value 15 predetermined.
    FIG. 4d illustrates by hatching the meshes which would have been validated on the date of (dd + 1) / mm / (YYYY - 10). According to FIG. 4d, only part of the meshes of the grid 11 would have been validated on the date of (dd + 1) / mm / (YYYY - 10), so that the processor 210 needs to continue the simulation. Thus, in the example of FIG. 4, for the third iteration of the simulation, the processor 210 takes into account the current date of iteration of (dd + 2) / mm / (YYYY - 10). Similarly, for the fourth iteration of the simulation, the processor 210 takes into account the current iteration date of (dd + 3) / mm / (YYYY - 10). And so on until the completion of the current simulation, that is to say, until each of the requested meshes Md is included in the 25 validated meshes Mv.
    Figure 4e illustrates by hatching the meshes which would have been validated at the end of the completion of a simulation.
    When all of the requested meshes Md are included in the validated meshes, the processor 210 implements step 150 in order to estimate the time taken to complete the request Rq for the past year considered.
    In one example, the time taken to complete the request Rq corresponds at least to the period elapsed since the date of initialization of the simulation of dd / mm / (YYYY - T) until the date on which the all the meshes would have been validated. For example, if T is equal to 10 as in the example above and the date of completion of simulation 35 is (dd + 5) / mm / (YYYY - 10), then the time taken to produce images satellite is six days. In another example, if T is equal to 10 as in the example above and the simulation completion date is (dd + 3) / (mm + 2) / (YYYY - 10), then the delay It takes two months and four days to produce satellite images. We can add to this delay other operational delays such as those necessary to carry out image processing operations, to download the mission plan from the mission center to the satellite.
    - 12 [0063] [0064] [0065] [0066] or also for downloading the images acquired by the observation satellite to the ground stations.
    In particular, it is planned to carry out a simulation for each of the years prior to the year associated with the start date of the analysis. In the example of figure 4, it could be a question of carrying out a simulation for each of the ten years previous to the year of the date of beginning of the request Rq. In a particular implementation, the processor 210 is configured to perform, in parallel, a plurality of simulations.
    In the case where several simulations are carried out, the processor 210 is further configured to determine at least one statistical quantity and / or at least one posterior probability from the completion times obtained during each of the simulated years.
    In one example, the statistical quantity includes the calculation of one of the following quantities, taken individually or according to any possible combination: an average, a weighted average, a median, a number of occurrences above or below a reference value, a maximum, a minimum, a standard deviation or the difference between a maximum and a minimum.
    In another example, the posterior probability is determined on the basis of the statistical quantity or a series of statistical quantities. Thus, for example, it is possible to estimate the probability of acquiring the satellite images associated with an imagery request, for one or more given completion times. In another example, we can determine the completion times for an imaging request for which the posterior probability is greater than a predetermined completion time determination threshold. FIG. 5 illustrates in the form of a histogram, a distribution of the completion time associated with a request Rq, and this, according to a plurality of simulated years. The histogram of FIG. 5 includes on the abscissa the completion time Dr expressed in days and includes on the ordinate the frequency of occurrence of the completion times, expressed as a percentage. Thus, in Figure 5, we can see that the probability of carrying out the request Rq in thirty days is greater than the probability of carrying it out in sixty days. In the example in FIG. 5, a threshold for determining the completion time set at 20% makes it possible to identify the period of thirty days as being the most likely for the completion of the request Rq.
    In addition, it is also envisaged to perform a simulation only for the years prior to the year associated with the start date which have meteorological similarities with the year associated with the start date. For example, it is known that climatic phenomena such as El Nino or La Nina are characterized by a particular chronology which can be predicted thanks to a coupling of the atmosphere and the surface ocean.
    In the claims, the term "include" does not exclude other elements or steps. The various characteristics presented and / or claimed may be [0067]
    - 13 advantageously combined. Their presence in the description or in different dependent claims does not exclude this possibility. Finally, the signs referring to the drawings should not be understood as limiting the scope of the invention.
    权利要求:
    Claims (11)
    [1" id="c-fr-0001]
    claims
    1. Method (100) for simulating the estimation of a delay in producing satellite images associated with at least one predetermined area of the Earth (20), by at least one Earth observation satellite comprising a system of optical imaging, the predetermined area being previously divided (110) according to a mesh grid (11), the acquisition being scheduled to be triggered from a start date of analysis, the method comprising the steps consisting in:
    (a) selecting (120) a plurality of grid cells, intended to be overflown by the satellite on a current iteration date, from the orbital characteristics of the satellite on the current iteration date, so as to obtain candidate meshes, the current iteration date corresponding to a date around the start date of analysis in a year prior to the year associated with the start date of analysis, (b) identify (130) among the candidate meshes, from a satellite mission plan, those for which planning is planned for the acquisition of at least one satellite image, so as to obtain planned meshes, (c) obtain (140) at least a first cloud value for each of the planned meshes, the first cloud value corresponding to an observation and / or a weather forecast, respectively observed on the current date of iteration ion or performed for the current iteration date, (d) identify (140) among the planned meshes, those for which the first associated cloudiness value is beyond a predetermined validation threshold value, so as to obtain validated meshes, (e) repeat steps (a) to (d), one or more times until each of the meshes of said grid is included in the validated meshes, taking into account at each iteration the unidentified meshes as validated and a period following the current iteration date considered in the previous iteration, (f) determine (150) the time taken to produce satellite images from the number of iterations carried out in step (e) .
    [2" id="c-fr-0002]
    2. Method according to claim 1, in which,
    - step (a) further includes the steps of:
    - obtain (120) at least a second cloud value for each of the candidate cells, the second cloud value corresponding to a meteorological observation and / or a meteorological forecast, respectively observed on the current date of iteration or carried out for the current date iteration, and,
    - identify (120) among the candidate meshes, those for which the second associated cloudiness value is beyond a predetermined selection threshold value different from the predetermined validation threshold value.
    [3" id="c-fr-0003]
    3. Method according to the preceding claims, in which the predetermined selection threshold value and the predetermined validation threshold value correspond to a threshold value of clear sky percentage.
    [4" id="c-fr-0004]
    4. Method according to claim 3, in which the validation threshold value is greater than the selection threshold value.
    [5" id="c-fr-0005]
    5. Method according to the preceding claims, in which step (f) further comprises the step of determining at least one statistical quantity and / or at least one posterior probability from a plurality of completion times d 'satellite images determined in step (d).
    [6" id="c-fr-0006]
    6. A computer program product, which, when executed by a computer, is arranged to execute a method according to any one of the preceding claims; the computer program being, optionally, stored on a computer-readable medium.
    [7" id="c-fr-0007]
    7. Device (200) for simulating the estimation of a delay in producing satellite images associated with at least one predetermined area of the Earth (20), by at least one Earth observation satellite comprising a system of optical imaging, the predetermined area being previously divided according to a mesh grid (11), the acquisition being scheduled to be triggered from a start date of analysis, the device comprising:
    - a memory (210) configured to store:
    - the mesh grid associated with the predetermined area,
    - the orbital characteristics of the satellite at a current iteration date, the current iteration date corresponding to a date around the start date of analysis in a year prior to the year associated with the start date analysis, and
    - at least a first cloud value for each of the grid cells, the first cloud value corresponding to an observation and / or a weather forecast, respectively observed on the current date of iteration or carried out for the current date of iteration ,
    - a processor (220) coupled to the memory and configured to select a plurality of meshes of the grid, intended to be overflown by the satellite on the current date of iteration from the orbital characteristics of the satellite on the current date of iteration , so as to obtain candidate meshes, the processor being further configured for:
    (a) identify among the candidate meshes, from a satellite mission plan, those for which a planning of acquisition of at least one satellite image is planned, (b) identify among the candidate meshes, those for which the first associated cloudiness value is beyond a predetermined validation threshold value, so as to obtain planned meshes, (c) repeat operations (a) and (b), one or more times until each meshes of said grid is included in the validated meshes, taking into consideration at each iteration the meshes not identified as validated and a period following the current date of iteration considered in the previous iteration, (d) determining the delay for realization of satellite images from the number of iterations carried out during the operation (c).
    [8" id="c-fr-0008]
    8. Device according to claim 7, in which:
    the memory (210) is further configured to store a second cloud value for each of the candidate cells, the second cloud value corresponding to a meteorological observation and / or a meteorological forecast, respectively observed on the current date of iteration or performed for the current iteration date, and,
    the processor (220) is further configured to identify, among the candidate cells, those for which the second associated cloudiness value is beyond a predetermined selection threshold value different from the predetermined validation threshold value, so as to get the candidate stitches.
    [9" id="c-fr-0009]
    9. Device according to the preceding claims, in which the predetermined selection threshold value and the predetermined validation threshold value correspond to a threshold value of clear sky percentage.
    [10" id="c-fr-0010]
    10. Device according to claim 9, in which the validation threshold value is greater than the selection threshold value.
    [11" id="c-fr-0011]
    11. Device according to the preceding claims, in which the processor is further configured to determine, during the operation (d), at least one statistical quantity and / or at least one posterior probability from a plurality of deadlines for producing satellite images determined during the operation (c).
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    同族专利:
    公开号 | 公开日
    WO2019020499A1|2019-01-31|
    EP3658851A1|2020-06-03|
    FR3069651B1|2020-03-06|
    EP3658851B1|2021-10-06|
    US11106910B2|2021-08-31|
    US20200160029A1|2020-05-21|
    引用文献:
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    WO2011089477A1|2010-01-25|2011-07-28|Tarik Ozkul|Autonomous decision system for selecting target in observation satellites|
    FR3011322A1|2013-10-02|2015-04-03|Centre Nat Etd Spatiales|SYSTEM AND METHOD FOR THE GROUPING OF ACQUISITIONS|
    FR3039728A1|2015-07-28|2017-02-03|Airbus Defence & Space Sas|METHOD FOR PLANNING THE ACQUISITION OF IMAGES OF TERRESTRIAL AREAS BY A SPACE DEVICE|
    US10459119B2|2014-12-26|2019-10-29|Matthew Kuhns|System and method for predicting sunset vibrancy|
    US10345483B2|2015-06-10|2019-07-09|Escaype|Observer-based meteorology and image identification|
    US11181665B2|2015-11-25|2021-11-23|Board Of Trustees Of The University Of Alabama|Systems and methods for monitoring updrafts in clouds|FR3073280B1|2017-11-09|2020-08-28|Airbus Defence & Space Sas|TERRESTRIAL SURFACE OBSERVATION PROCESS AND DEVICE FOR ITS IMPLEMENTATION|
    FR3092565B1|2019-02-08|2021-08-27|Airbus Defence & Space Sas|Computer systems for the acquisition of satellite images taking into account meteorological uncertainty|
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    法律状态:
    2019-02-01| PLSC| Publication of the preliminary search report|Effective date: 20190201 |
    2019-07-29| PLFP| Fee payment|Year of fee payment: 3 |
    2020-07-24| PLFP| Fee payment|Year of fee payment: 4 |
    2021-06-28| PLFP| Fee payment|Year of fee payment: 5 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1757161|2017-07-27|
    FR1757161A|FR3069651B1|2017-07-27|2017-07-27|DEVICE AND METHOD FOR SIMULATING THE ESTIMATE OF A DELAY IN REALIZING SATELLITE IMAGES OF THE EARTH|FR1757161A| FR3069651B1|2017-07-27|2017-07-27|DEVICE AND METHOD FOR SIMULATING THE ESTIMATE OF A DELAY IN REALIZING SATELLITE IMAGES OF THE EARTH|
    EP18740244.1A| EP3658851B1|2017-07-27|2018-07-20|Device and method for simulating the estimation of a lag in producing satellite images of the earth|
    PCT/EP2018/069707| WO2019020499A1|2017-07-27|2018-07-20|Device and method for simulating the estimation of a lag in producing satellite images of the earth|
    US16/634,287| US11106910B2|2017-07-27|2018-07-20|Device and method for simulating the estimation of a lag in producing satellite images of the earth|
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