CN111598407B - System and method for planning carbon satellite task - Google Patents
System and method for planning carbon satellite task Download PDFInfo
- Publication number
- CN111598407B CN111598407B CN202010323318.9A CN202010323318A CN111598407B CN 111598407 B CN111598407 B CN 111598407B CN 202010323318 A CN202010323318 A CN 202010323318A CN 111598407 B CN111598407 B CN 111598407B
- Authority
- CN
- China
- Prior art keywords
- task
- planning
- observation
- sequence
- module
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 title claims abstract description 62
- 229910052799 carbon Inorganic materials 0.000 title claims abstract description 62
- 238000000034 method Methods 0.000 title claims abstract description 26
- 238000012795 verification Methods 0.000 claims abstract description 23
- 238000005286 illumination Methods 0.000 claims abstract description 8
- 230000002159 abnormal effect Effects 0.000 claims description 4
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06Q—INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR
- G06Q10/00—Administration; Management
- G06Q10/06—Resources, workflows, human or project management; Enterprise or organisation planning; Enterprise or organisation modelling
- G06Q10/063—Operations research, analysis or management
- G06Q10/0631—Resource planning, allocation, distributing or scheduling for enterprises or organisations
- G06Q10/06315—Needs-based resource requirements planning or analysis
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06Q—INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR
- G06Q10/00—Administration; Management
- G06Q10/06—Resources, workflows, human or project management; Enterprise or organisation planning; Enterprise or organisation modelling
- G06Q10/063—Operations research, analysis or management
- G06Q10/0631—Resource planning, allocation, distributing or scheduling for enterprises or organisations
- G06Q10/06316—Sequencing of tasks or work
-
- G06Q50/40—
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A90/00—Technologies having an indirect contribution to adaptation to climate change
- Y02A90/10—Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation
Abstract
The application discloses a system and a method for planning a carbon satellite task, wherein the system comprises a parameter setting module, a parameter setting module and a parameter analysis module, wherein the parameter setting module is used for configuring various parameters required by target observation, daily calibration, lunar calibration, a directing mirror and flare observation tasks; the data loading module is used for loading a track data file, an illumination characteristic file and a target observation characteristic file which are required by task planning; the task sequence planning module is used for observing tasks of the carbon satellite and executing different orientations and switching among the tasks; the task sequence verification module is used for verifying the task sequence planned by the task sequence planning module by task planning constraint, so as to ensure that the task sequence meets constraint conditions; and the task sequence generation module is used for generating a task sequence file for the pointing sequence generation system to use when the task sequence planned by the system passes the verification, otherwise, alarming.
Description
Technical Field
The application relates to the technical field of carbon satellite observation, in particular to a system and a method for planning a carbon satellite mission.
Background
The satellite resources are valuable, satellite performance is fully utilized, task planning is needed to be conducted on the satellite to maximize the utilization of the satellite resources, in the task planning process, due to the fact that the satellite resources are limited, the task planning needs to consider many constraints, the satellite greatly improves the working level along with the improvement of the attitude mechanical capacity and the load performance of the satellite, but meanwhile, the energy consumption of the satellite is increased, the satellite energy tasks are needed to be effectively planned, and the situation that the satellite is insufficient in energy source when the satellite performs the tasks is prevented, so that the satellite faults and the tasks cannot be completed smoothly.
Disclosure of Invention
Aiming at the technical problems in the related art, the application provides a system and a method for planning the mission of a carbon satellite, which can edit a satellite working mode into an effective mission sequence so as to meet the observation requirement and the calibration requirement of the satellite, ensure the effectiveness of satellite observation data and improve the calibration precision of the satellite observation data.
In order to achieve the technical purpose, the technical scheme of the application is realized as follows: a system for carbon satellite mission planning, the system comprising:
the parameter setting module is used for configuring various parameters required by target observation, daily calibration, monthly calibration, pointing mirror and flare observation tasks;
the data loading module is used for loading a track data file, an illumination characteristic file and a target observation characteristic file which are required by task planning;
the task sequence planning module is used for observing tasks of the carbon satellite and executing different orientations and switching among the tasks;
the task sequence verification module is used for verifying the task sequence planned by the task sequence planning module by task planning constraint so as to ensure that the task sequence meets constraint conditions;
and the task sequence generation module is used for generating a task sequence file for the pointing sequence generation system to use when the task sequence planned by the system passes the verification, and otherwise, alarming is carried out.
Further, the task sequence planning module plans the working mode of the carbon satellite by taking each orbit as a unit according to the task characteristics, determines the task sequence of the satellite in one orbit according to the main carbon observation task and the main pointing mode of the satellite in the one orbit, and timely selects one orbit to execute the carbon load positioning task according to the requirements and conditions.
Further, the task sequence planning module plans the task sequence of all orbits in the day based on the carbon satellite task planning module according to the observation task demand and task planning constraint and by combining the parameters provided by the parameter setting module and the files provided by the data loading module.
Further, the task sequence executed by the task sequence planning module includes:
(1) Flare, task code t_r1;
(2) Flare + Z axis pair day scale, task code t_r2;
(3) The flare + X axis pair is scaled, task code t_r3;
(4) Flare + versus month scale, task code t_r4;
(5) The zenith main plane and the task code number T_Z1;
(6) Daily calibration and task code number T_Z2 are carried out on the principal plane of the nadir and the Z axis;
(7) Day calibration and task code number T_Z3 are carried out on the sun-bottom main plane and the X axis;
(8) The zenith principal plane + month scaling and task code t_z4;
(9) The nadir is not a main plane, and the task code number T_N1;
(10) The nadir non-principal plane + month scaling, task code t_n2;
(11) Target + gaze, task code t_o1;
(12) Target + region, task designation t_o2.
Further, the constraint conditions of the task sequence verification module include:
where, if t_ni=t_rj (j=1, 2,3, 4), then t_n (i-1) =t_zk (k=1, 2,3, 4), t_n (i+1) =t_zs (s=1, 2,3, 4);
where, if t_ni=t_nj (j=1, 2), then t_n (i-1) =t_zk (k=1, 2,3, 4), t_n (i+1) =t_zs (s=1, 2,3, 4);
or t_n (i-1) =t_rk (k=1, 2,3, 4), t_n (i+1) =t_rs (s=1, 2,3, 4);
where, if t_ni=t_oj (j=1, 2), then t_n (i-1) =t_zk (k=1, 2,3, 4), t_n (i+1) =t_zs (s=1, 2,3, 4);
or t_n (i-1) =t_rk (k=1, 2,3, 4), t_n (i+1) =t_rs (s=1, 2,3, 4);
where tjn1=t_zj (j=1, 2,3, 4);
wherein, T_R2, T_Z2 at most once a day;
wherein, T_R3, T_Z3 at most once a month;
wherein CO2 has an internal scale and only one rail and is on the same rail as t_rj (j=1, 2,3, 4) or t_zj (j=1, 2,3, 4);
where Num represents the total number of orbits of the carbon satellites on the day of mission planning, i=2, 3, …, and Num, T represents the day.
Further, the task sequence planning of the task sequence generating module specifically includes:
firstly, judging whether an application track of target observation needs and target observation exists, and configuring a task of a selected track as target observation T_Oj (j=1, 2);
then, the first track task is planned as t_zj (j=1, 2,3, 4);
secondly, task configuration is carried out on tasks of the remaining tracks track by track according to task planning constraints, and the specific constraints correspond to the task sequence verification module;
finally, a track is selected from tracks with a task plan of t_rj (j=1, 2,3, 4) or t_zj (j=1, 2,3, 4) for CO2 in-scaling.
A method for planning a mission of a carbon satellite, the method comprising the steps of:
s1: effectively arranging and combining the observation tasks of the carbon satellite, generating an effective task sequence, and realizing the effective combination of various observation tasks;
s2: and according to the observation task requirements and task planning constraints, combining the parameter data files and the specific files, drawing task sequences of all orbits in one day according to the regulations of a carbon satellite task planning party, checking the task sequences, generating task sequence files after checking, and transmitting the task sequence files to a pointing sequence generating system by using a network for satellite use.
Further, the step S1 includes the steps of:
s1.1 carbon satellite observation tasks comprise a zenith principal plane observation, a flare observation, a zenith non-principal plane observation, CO2 internal calibration, target observation, hot spot area observation, Z-axis daily calibration, X-axis daily calibration and month calibration, and the observation tasks are effectively arranged and combined to generate an effective task sequence.
Further, the step S2 includes the steps of:
s2.1: parameter configuration is carried out on target observation, daily calibration, month calibration and flare observation according to observation requirements, and the rotation angle of the pointing mirror is configured according to the requirements of the angle of the pointing mirror in each pointing mode;
s2.2: automatically acquiring a track data file, an illumination characteristic file and a target observation characteristic file from a designated position at regular daily time by the system;
s2.3: task sequence planning automatically calculates a target observable track according to parameter setting and the acquired data file for selection by a user;
s2.4: after a user determines a target observation task, the user autonomously selects a corresponding track to observe the target, and simultaneously performs task sequence planning on other tracks on the same day according to task planning constraint;
s2.5: configuring the CO2 internal calibration task into a corresponding task sequence to complete task sequence planning;
s2.6: after the task sequence planning is completed, automatically checking by the system, and feeding back a checking result to a user;
s2.7: and after the verification is passed, automatically transmitting the planned task sequence to a pointing sequence generating system, and if the verification is not passed, returning to the target observation according to the abnormal information to carry out task sequence planning again.
Further, the step S1.1 includes the steps of:
scaling is carried out on the basis of CO2 once a day, and the scaling is carried out through optional one track in a zenith principal plane observation or flare observation track by observation requirements and on-board energy source limitation.
The application has the beneficial effects that: in view of the fact that a planning method specially aiming at a carbon satellite observation task does not exist in the prior art, as the carbon satellite observation requirements are various and the carbon satellite observation modes are complicated and various, the method edits the carbon satellite working modes into an effective task sequence, meets the observation requirement and the calibration requirement of the carbon satellite, ensures the effectiveness of carbon satellite observation data, improves the calibration precision of the carbon satellite observation data, realizes the task planning of the carbon satellite, and automatically sends the generated task sequence to a pointing sequence generating system through a network for the carbon satellite to use.
Drawings
In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings that are needed in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present application, and other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
FIG. 1 is a block diagram of a system and method for carbon satellite mission planning in accordance with an embodiment of the present application;
fig. 2 is a flow chart of a system and method for carbon satellite mission planning according to an embodiment of the present application.
Detailed Description
The following description of the embodiments of the present application will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present application, but not all embodiments. All other embodiments, which are derived by a person skilled in the art based on the embodiments of the application, fall within the scope of protection of the application.
As shown in fig. 1-2, a system and a method for planning a mission of a carbon satellite according to an embodiment of the present application, the system includes:
the parameter setting module is used for configuring various parameters required by target observation, daily calibration, monthly calibration, pointing mirror and flare observation tasks, and the data loading module is used for loading track data files, illumination characteristic files and target observation characteristic files required by task planning;
the task sequence planning module performs the task sequence of the satellite in one track according to the main carbon observation task and the main pointing mode of the satellite in one track, and timely selects the one track to execute the carbon load calibration task according to the requirement and the condition, performs the task planning constraint according to the observation task requirement and the task planning constraint, combines the parameters provided by the parameter setting module and the files provided by the data loading module, and marks the task sequence of all the tracks in one day according to the regulation of the task planning party of the carbon satellite, wherein the task sequence executed in one track comprises:
(1) Flare, task code t_r1;
(2) Flare + Z axis pair day scale, task code t_r2;
(3) The flare + X axis pair is scaled, task code t_r3;
(4) Flare + versus month scale, task code t_r4;
(5) The zenith main plane and the task code number T_Z1;
(6) Daily calibration and task code number T_Z2 are carried out on the principal plane of the nadir and the Z axis;
(7) Day calibration and task code number T_Z3 are carried out on the sun-bottom main plane and the X axis;
(8) The zenith principal plane + month scaling and task code t_z4;
(9) The nadir is not a main plane, and the task code number T_N1;
(10) The nadir non-principal plane + month scaling, task code t_n2;
(11) Target + gaze, task code t_o1;
(12) Target + region, task designation t_o2.
In one embodiment of the present application,
the task sequence verification module is used for verifying a task sequence planned by the task sequence planning module by task planning constraint, ensuring that the task sequence meets constraint conditions and is used for:
where, if t_ni=t_rj (j=1, 2,3, 4), then t_n (i-1) =t_zk (k=1, 2,3, 4), t_n (i+1) =t_zs (s=1, 2,3, 4);
where, if t_ni=t_nj (j=1, 2), then t_n (i-1) =t_zk (k=1, 2,3, 4), t_n (i+1) =t_zs (s=1, 2,3, 4);
or t_n (i-1) =t_rk (k=1, 2,3, 4), t_n (i+1) =t_rs (s=1, 2,3, 4);
where, if t_ni=t_oj (j=1, 2), then t_n (i-1) =t_zk (k=1, 2,3, 4), t_n (i+1) =t_zs (s=1, 2,3, 4);
or t_n (i-1) =t_rk (k=1, 2,3, 4), t_n (i+1) =t_rs (s=1, 2,3, 4);
where tjn1=t_zj (j=1, 2,3, 4);
wherein, T_R2, T_Z2 at most once a day;
wherein, T_R3, T_Z3 at most once a month;
wherein CO2 has an internal scale and only one rail and is on the same rail as t_rj (j=1, 2,3, 4) or t_zj (j=1, 2,3, 4);
wherein Num represents the total number of orbits of the carbon satellites on the day of mission planning, i=2, 3, …, and Num, T represents the day;
the task sequence generation module is used for generating a task sequence file for the pointed sequence generation system to use when the task sequence planned by the system passes the verification, otherwise, alarming is carried out, and the task sequence generation module is used for:
firstly, judging whether an application track of target observation needs and target observation exists, and configuring a task of a selected track as target observation T_Oj (j=1, 2);
then, the first track task is planned as t_zj (j=1, 2,3, 4);
secondly, task configuration is carried out on tasks of the remaining tracks track by track according to task planning constraints, and the specific constraints correspond to the task sequence verification module;
finally, a track is selected from tracks with a task plan of t_rj (j=1, 2,3, 4) or t_zj (j=1, 2,3, 4) for CO2 in-scaling.
A method for planning a mission of a carbon satellite, the method comprising the steps of:
s1: the method comprises the following steps of (1) effectively arranging and combining the observation tasks of a carbon satellite, generating an effective task sequence, and realizing effective combination of various observation tasks, wherein the carbon satellite observation tasks comprise a zenith main plane observation, a flare observation, a zenith non-main plane observation, a CO2 internal calibration, a target observation, a hot spot area observation, a Z-axis daily calibration, an X-axis daily calibration and a month calibration, and are used for effectively arranging and combining the observation tasks and generating an effective task sequence, wherein the CO2 internal calibration is carried out once a day, and is limited by observation requirements and on-board energy sources, and is carried out through an optional orbit in a zenith main plane observation or a flare observation orbit;
s2: and planning a carbon satellite task, namely planning task sequences of all orbits in one day according to the requirements of an observation task and task planning constraints, combining parameter files and specific files, checking the task sequences, generating task sequence files after checking, transmitting the task sequence files to a pointing sequence generating system by using a network, and providing the satellite with the method, wherein the method further comprises the following steps of:
s2.1: parameter configuration is carried out on target observation, daily calibration, month calibration and flare observation according to observation requirements, and the rotation angle of the pointing mirror is configured according to the requirements of the angle of the pointing mirror in each pointing mode;
s2.2: automatically acquiring a track data file, an illumination characteristic file and a target observation characteristic file from a designated position at regular daily time by the system;
s2.3: task sequence planning automatically calculates a target observable track according to parameter setting and the acquired data file for selection by a user;
s2.4: after a user determines a target observation task, the user autonomously selects a corresponding track to observe the target, and simultaneously performs task sequence planning on other tracks on the same day according to task planning constraint;
s2.5: configuring the CO2 internal calibration task into a corresponding task sequence to complete task sequence planning;
s2.6: after the task sequence planning is completed, automatically checking by the system, and feeding back a checking result to a user;
s2.7: and after the verification is passed, automatically transmitting the planned task sequence to a pointing sequence generating system, and if the verification is not passed, returning to the target observation according to the abnormal information to carry out task sequence planning again.
In a specific embodiment of the present application, the S2.4 task sequence planning includes the following steps:
s2.4.1 flare, task code T_R1;
s2.4.2 flare+Z axis pair day scale, task code T_R2;
s2.4.3 flare+X axis pair day scale, task code T_R3;
s2.4.4 flare + scale for month, task code t_r4;
s2.4.5 day bottom principal plane, task code t_z1;
s2.4.6 day bottom principal plane+Z axis pair day scale, task code T_Z2;
the S2.4.7 day bottom main plane and the X axis are subjected to daily calibration, and the task code number T_Z3;
s2.4.8 day bottom principal plane + month scale, task code t_z4;
s2.4.9 days bottom non-principal plane, task code t_n1;
s2.4.10 non-principal plane at day bottom + month scale, task code t_n2;
s2.4.11 target+gaze, task code t_o1;
s2.4.12 target + region, task designation t_o2.
In a specific embodiment of the present application, the S2.6 automatic verification includes the following steps:
s2.6.1 when t_ni=t_rj (j=1, 2,3, 4), t_n (i-1) =t_zk (k=1, 2,3, 4), t_n (i+1) =t_zs (s=1, 2,3, 4);
s2.6.2 when t_ni=t_nj (j=1, 2), t_n (i-1) =t_zk (k=1, 2,3, 4), t_n (i+1) =t_zs (s=1, 2,3, 4);
or t_n (i-1) =t_rk (k=1, 2,3, 4), t_n (i+1) =t_rs (s=1, 2,3, 4);
s2.6.3 when t_ni=t_oj (j=1, 2), t_n (i-1) =t_zk (k=1, 2,3, 4), t_n (i+1) =t_zs (s=1, 2,3, 4);
or t_n (i-1) =t_rk (k=1, 2,3, 4), t_n (i+1) =t_rs (s=1, 2,3, 4);
S2.6.4 T_N1= T_Zj(j=1,2,3,4)；
s2.6.5 has a maximum of once a day T_R2, T_Z2;
s2.6.6 has a maximum of once a month T_R3, T_Z3;
s2.6.7 CO2 has an internal calibration and only one track, and is on the same track as t_rj (j=1, 2,3, 4) or t_zj (j=1, 2,3, 4);
where Num represents the total number of orbits of the carbon satellites on the day of mission planning, i=2, 3, …, and Num, T represents the day.
In a specific embodiment of the present application, the step S2.7 includes the steps of:
s2.7.1 determining whether there is a target observation requirement and an application track of the target observation, and configuring the task of the selected track as a target observation t_oj (j=1, 2);
s2.7.2 first track task is specified as t_zj (j=1, 2,3, 4);
s2.7.3 carrying out task configuration on tasks of the remaining tracks track by track according to task planning constraints, wherein specific constraints correspond to the task sequence verification module;
s2.7.4 a track is selected from tracks with task plans t_rj (j=1, 2,3, 4) or t_zj (j=1, 2,3, 4) for CO2 intra scaling.
In order to facilitate understanding of the above technical solutions of the present application, the following describes the above technical solutions of the present application in detail by a specific usage manner.
When the system and the method for planning the carbon satellite task are particularly used, the carbon satellite observation tasks are effectively arranged and combined, an effective task sequence is generated, and the effective combination of various observation tasks is realized; the carbon satellite task planning, according to the observation task demand and task planning constraint, combines the parameter file and the specific file, and according to the rules of the carbon satellite task planning party, the task sequence of all orbits in one day is planned, and is checked, the task sequence file is generated after the checking, the task sequence file is sent to the pointing sequence generating system by using the network, and the method further comprises the following steps:
firstly, carrying out parameter configuration on target observation, daily calibration, month calibration and flare observation according to observation requirements, and configuring the rotation angle of a pointing mirror according to the requirements of the angle of the pointing mirror in each pointing mode;
step two, automatically acquiring a track data file, an illumination characteristic file and a target observation characteristic file from a designated position at regular daily time by the system;
step three, task sequence planning automatically calculates a target observable track according to parameter setting and the acquired data file for selection by a user;
step four, after the user determines a target observation task, the user autonomously selects a corresponding track to observe the target, and simultaneously performs task sequence planning on other tracks on the same day according to task planning constraint;
fifthly, configuring the CO2 internal positioning task into a corresponding task sequence to complete task sequence planning;
step six, after the task sequence planning is completed, automatically checking by the system, and feeding back a checking result to a user;
and step seven, after the verification is passed, automatically sending the planned task sequence to a pointing sequence generating system, and if the verification is not passed, returning to the target observation according to the abnormal information to carry out task sequence planning again.
In summary, by means of the above technical solution of the present application, because of the diversity of the observation requirements of the carbon satellite, a complex and diverse observation mode is designed for the carbon satellite, and in order to effectively control various modes of the carbon satellite and ensure the observation requirement and calibration requirement of the satellite, the present application designs an effective carbon satellite mission planning system and method to realize mission planning of the carbon satellite.
The foregoing description of the preferred embodiments of the application is not intended to be limiting, but rather is intended to cover all modifications, equivalents, alternatives, and improvements that fall within the spirit and scope of the application.
Claims (7)
1. A system for carbon satellite mission planning, the system comprising:
the parameter setting module is used for configuring various parameters required by target observation, daily calibration, monthly calibration, pointing mirror and flare observation tasks;
the data loading module is used for loading a track data file, an illumination characteristic file and a target observation characteristic file which are required by task planning;
the task sequence planning module is used for observing tasks of the carbon satellite and executing switching among different directions and tasks, the task sequence planning module combines parameters provided by the parameter setting module and files provided by the data loading module according to requirements of the observed tasks and task planning constraints, and the task sequence of the task sequence planning module is based on the task sequence of all orbits in the day, and specifically comprises the following steps:
(1) Flare, task code t_r1;
(2) Flare + Z axis pair day scale, task code t_r2;
(3) The flare + X axis pair is scaled, task code t_r3;
(4) Flare + versus month scale, task code t_r4;
(5) The zenith main plane and the task code number T_Z1;
(6) Daily calibration and task code number T_Z2 are carried out on the principal plane of the nadir and the Z axis;
(7) Day calibration and task code number T_Z3 are carried out on the sun-bottom main plane and the X axis;
(8) The zenith principal plane + month scaling and task code t_z4;
(9) The nadir is not a main plane, and the task code number T_N1;
(10) The nadir non-principal plane + month scaling, task code t_n2;
(11) Target + gaze, task code t_o1;
(12) Target + region, task code t_o2;
the task sequence verification module is used for verifying a task sequence planned by the task sequence planning module by task planning constraint so as to ensure that the task sequence meets constraint conditions, and the constraint conditions of the task sequence verification module comprise:
where, if t_ni=t_rj (j=1, 2,3, 4), then t_n (i-1) =t_zk (k=1, 2,3, 4), t_n (i+1) =t_zs (s=1, 2,3, 4);
where, if t_ni=t_nj (j=1, 2), then t_n (i-1) =t_zk (k=1, 2,3, 4), t_n (i+1) =t_zs (s=1, 2,3, 4);
or t_n (i-1) =t_rk (k=1, 2,3, 4), t_n (i+1) =t_rs (s=1, 2,3, 4);
where, if t_ni=t_oj (j=1, 2), then t_n (i-1) =t_zk (k=1, 2,3, 4), t_n (i+1) =t_zs (s=1, 2,3, 4);
or t_n (i-1) =t_rk (k=1, 2,3, 4), t_n (i+1) =t_rs (s=1, 2,3, 4);
where tjn1=t_zj (j=1, 2,3, 4);
wherein, T_R2, T_Z2 at most once a day;
wherein, T_R3, T_Z3 at most once a month;
wherein CO 2 With internal calibration and only one track, and on the same track as t_rj (j=1, 2,3, 4) or t_zj (j=1, 2,3, 4);
wherein Num represents the total number of orbits of the carbon satellites on the day of mission planning, i=2, 3, …, and Num, T represents the day;
and the task sequence generation module is used for generating a task sequence file for the pointing sequence generation system to use when the task sequence planned by the system passes the verification, and otherwise, alarming is carried out.
2. The system of claim 1, wherein the mission sequence planning module plans the working mode of the carbon satellite in each orbit according to the mission characteristics, determines the mission sequence of the satellite in the orbit according to the main carbon observation mission and the main pointing mode of the satellite in the orbit, and timely selects an orbit to execute the carbon load calibration mission according to the requirements and conditions.
3. The system for planning a mission of a carbon satellite of claim 1, wherein the mission sequence generation module comprises:
firstly, judging whether an application track of target observation needs and target observation exists, and configuring a task of a selected track as target observation T_Oj (j=1, 2);
then, the first track task is planned as t_zj (j=1, 2,3, 4);
secondly, task configuration is carried out on tasks of the remaining tracks track by track according to task planning constraints, and the specific constraints correspond to the task sequence verification module;
finally, a track is selected from tracks with a task specification of t_rj (j=1, 2,3, 4) or t_zj (j=1, 2,3, 4) for CO 2 And (5) internal scaling.
4. A method for planning a mission of a carbon satellite, the method comprising the steps of:
s1: effectively arranging and combining the observation tasks of the carbon satellite, generating an effective task sequence, and realizing the effective combination of various observation tasks;
s2: and according to the requirements of the observation task and the task planning constraint, the task sequences of all orbits in one day are marked out according to the regulations of the carbon satellite task planning party by combining the parameters provided by the parameter setting module and the files provided by the data loading module, the task sequences are checked, the task sequence files are generated after the checking, and the task sequence files are sent to the pointing sequence generating system by using a network for use by satellites.
5. The method of carbon satellite mission planning of claim 4, wherein S1 comprises the steps of:
s1.1 carbon satellite observation tasks comprise a zenith principal plane observation, a flare observation, a zenith non-principal plane observation and CO 2 Internal calibration, target observation, hot spot observation, Z-axis daily calibration, X-axis daily calibration and monthly calibration, and effectively arranging and combining observation tasks to generate an effective taskSequence.
6. The method of carbon satellite mission planning of claim 4, wherein S2 comprises the steps of:
s2.1: parameter configuration is carried out on target observation, daily calibration, month calibration and flare observation according to observation requirements, and the rotation angle of the pointing mirror is configured according to the requirements of the angle of the pointing mirror in each pointing mode;
s2.2: automatically acquiring a track data file, an illumination characteristic file and a target observation characteristic file from a designated position at regular daily time by the system;
s2.3: task sequence planning automatically calculates a target observable track according to parameter setting and the acquired data file for selection by a user;
s2.4: after a user determines a target observation task, the user autonomously selects a corresponding track to observe the target, and simultaneously performs task sequence planning on other tracks on the same day according to task planning constraint;
s2.5: CO is processed by 2 The internal calibration tasks are configured into corresponding task sequences, and task sequence planning is completed;
s2.6: after the task sequence planning is completed, automatically checking by the system, and feeding back a checking result to a user;
s2.7: and after the verification is passed, automatically transmitting the planned task sequence to a pointing sequence generating system, and if the verification is not passed, returning to the target observation according to the abnormal information to carry out task sequence planning again.
7. The method of carbon satellite mission planning of claim 4, wherein S1.1 comprises the steps of:
based on CO 2 The internal calibration is carried out once a day, limited by the observation requirement and the energy source on the satellite, and is carried out by selecting one track in the observation track of the principal plane of the sky or the flare.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010323318.9A CN111598407B (en) | 2020-04-22 | 2020-04-22 | System and method for planning carbon satellite task |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010323318.9A CN111598407B (en) | 2020-04-22 | 2020-04-22 | System and method for planning carbon satellite task |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN111598407A CN111598407A (en) | 2020-08-28 |
| CN111598407B true CN111598407B (en) | 2023-09-01 |
Family
ID=72181650
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010323318.9A Active CN111598407B (en) | 2020-04-22 | 2020-04-22 | System and method for planning carbon satellite task |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN111598407B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA3213349A1 (en) * | 2021-07-12 | 2023-01-19 | Longfei TIAN | Autonomous mission planning method for carbon satellite |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102520619A (en) * | 2011-11-15 | 2012-06-27 | 上海卫星工程研究所 | General-purpose satellite remote sensing simulator |
| CN105095643A (en) * | 2015-06-15 | 2015-11-25 | 中国人民解放军国防科学技术大学 | Method for planning autonomous task of imaging satellite in dynamic environment |
| CN106022586A (en) * | 2016-05-13 | 2016-10-12 | 中国人民解放军国防科学技术大学 | Satellite observation task planning method based on case matching |
| CN106570614A (en) * | 2016-10-14 | 2017-04-19 | 上海微小卫星工程中心 | Onboard autonomous distributed task scheduling method |
| CN106611292A (en) * | 2016-12-20 | 2017-05-03 | 中国电子科技集团公司第五十四研究所 | Satellite task planning method based on configurable general constraint handling rule |
| CN107016095A (en) * | 2017-04-07 | 2017-08-04 | 北京理工大学 | Climate change comprehensive estimation method based on multi-source carbon number evidence |
| CN108388958A (en) * | 2018-01-31 | 2018-08-10 | 中国地质大学（武汉） | A kind of method and device of two-dimensional attitude maneuvering satellite mission planning technical research |
| CN110161533A (en) * | 2019-06-17 | 2019-08-23 | 国家卫星气象中心(国家空间天气监测预警中心) | Unattended satellite optical load intelligence spectral radiometric calibration system |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7020697B1 (en) * | 1999-10-01 | 2006-03-28 | Accenture Llp | Architectures for netcentric computing systems |
| US20120078931A1 (en) * | 2010-09-29 | 2012-03-29 | International Business Machines Corporation | Methods for managing ownership of redundant data and systems thereof |
| US9031585B2 (en) * | 2011-11-29 | 2015-05-12 | Trimble Navigation Limited | Integrating position information into a handheld tool |
-
2020
- 2020-04-22 CN CN202010323318.9A patent/CN111598407B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102520619A (en) * | 2011-11-15 | 2012-06-27 | 上海卫星工程研究所 | General-purpose satellite remote sensing simulator |
| CN105095643A (en) * | 2015-06-15 | 2015-11-25 | 中国人民解放军国防科学技术大学 | Method for planning autonomous task of imaging satellite in dynamic environment |
| CN106022586A (en) * | 2016-05-13 | 2016-10-12 | 中国人民解放军国防科学技术大学 | Satellite observation task planning method based on case matching |
| CN106570614A (en) * | 2016-10-14 | 2017-04-19 | 上海微小卫星工程中心 | Onboard autonomous distributed task scheduling method |
| CN106611292A (en) * | 2016-12-20 | 2017-05-03 | 中国电子科技集团公司第五十四研究所 | Satellite task planning method based on configurable general constraint handling rule |
| CN107016095A (en) * | 2017-04-07 | 2017-08-04 | 北京理工大学 | Climate change comprehensive estimation method based on multi-source carbon number evidence |
| CN108388958A (en) * | 2018-01-31 | 2018-08-10 | 中国地质大学（武汉） | A kind of method and device of two-dimensional attitude maneuvering satellite mission planning technical research |
| CN110161533A (en) * | 2019-06-17 | 2019-08-23 | 国家卫星气象中心(国家空间天气监测预警中心) | Unattended satellite optical load intelligence spectral radiometric calibration system |
Non-Patent Citations (1)
| Title |
|---|
| 面向多星任务规划问题的改进遗传算法;宋彦杰;《控制理论与应用》;第36卷(第9期);1391-1397 * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN111598407A (en) | 2020-08-28 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Du et al. | A new multi-satellite autonomous mission allocation and planning method | |
| CN111598407B (en) | System and method for planning carbon satellite task | |
| CN112465296B (en) | Dynamic task re-planning method for agile satellite | |
| CN108462467B (en) | Solar wing on-orbit output power evaluation method | |
| CN106570614A (en) | Onboard autonomous distributed task scheduling method | |
| CN106742086A (en) | Quick imaging satellite independently transports control system | |
| Stephens | The Juno mission to Jupiter: Lessons from cruise and plans for orbital operations and science return | |
| Bradley et al. | Europa Clipper mission: system integration review report | |
| Much et al. | The INTEGRAL ground segment and its science operations centre | |
| US20210078733A1 (en) | Lunar orbiting satellite system, and ground station of lunar orbiting satellite system | |
| Lessac-Chenen et al. | Lucy Optical Navigation Performance During The (152830) Dinkinesh Encounter | |
| KR100513059B1 (en) | Communications satellite system by two-stable and one equilibrium orbit satellites in the earth-moon and the method of tracing communications satellite system | |
| KR20030056471A (en) | a | |
| Williams et al. | Navigation for the MESSENGER Mission's First Mercury Encounter | |
| Wagner et al. | Communicating Navigation Data Inside the Cassini-Huygens Project: Visualizations and Tools | |
| Antreasian et al. | Orbit determination processes for the navigation of the Cassini-Huygens mission | |
| Madni et al. | Missed Thrust Requirements for Psyche Mission | |
| CN114926021B (en) | Satellite time sequence optimal task planning method based on integration of imaging segmentation and planning | |
| US11418064B1 (en) | System and method for providing disjointed space-based power beaming | |
| Spörl et al. | Mission planning system for the TET-1 OnOrbitVerification mission | |
| Peterson et al. | K2 Mission Operations: Finding Balance in Year One | |
| Carraway et al. | Lessons Learned from Clementine on the Way to Pluto | |
| Gaffney et al. | A reevaluation of selected mobile satellite communications systems: Ellipso; Globalstar, IRIDIUM and Odyssey | |
| KR100618655B1 (en) | Apparatus and method for automated station keeping of geostationary satellite | |
| Ellery et al. | A proposed public-private partnership for the funding of robotic in-orbit servicers |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |