CN111598407A - Carbon satellite task planning system and method - Google Patents
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Abstract
The invention 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 setting module, wherein the parameter setting module is used for configuring various parameters required by target observation, daily calibration, monthly calibration, a directional mirror and a flare observation task; the data loading module is used for loading a track data file, an illumination characteristic file and a target observation characteristic file 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 checking module is used for checking the task sequence planned by the task sequence planning module by task planning constraint 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, or else, giving an alarm.
Description
Technical Field
The invention relates to the technical field of carbon satellite observation, in particular to a system and a method for carbon satellite task planning.
Background
The satellite is high in cost and precious in resource, so that the satellite efficiency is exerted to the maximum extent by fully utilizing satellite-ground resources, the satellite is required to be subjected to task planning to maximally utilize the satellite resources, in the task planning process, the satellite is limited in resource and many constraints are required to be considered in the task planning, along with the improvement of the satellite attitude maneuverability and load performance, the working level of the satellite is greatly improved, but the energy consumption of the satellite is increased, the satellite energy task is required to be effectively planned, and the situation that the satellite is insufficient in energy when the satellite executes the task is prevented, so that the satellite fault and the task cannot be smoothly completed.
Disclosure of Invention
Aiming at the technical problems in the related art, the invention provides a system and a method for planning a carbon satellite task, which can edit a satellite working mode into an effective task sequence so as to meet the observation requirement and the calibration requirement of a 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 invention 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, sun calibration, moon calibration, a directional 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 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 checking module is used for checking 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, or else, giving an alarm.
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 the orbit according to the main carbon observation task and the main pointing mode of the satellite in the orbit, and timely selects one orbit to execute the calibration task in the carbon load according to the requirement and the condition.
Further, the task sequence planning module plans the task sequences of all the orbits in one day based on the carbon satellite task planning module according to the observation task requirements and the task planning constraints 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) the flare + Z axis is calibrated to the day, and the task code is T _ R2;
(3) flare + X-axis daily calibration, task code T _ R3;
(4) flare + monthly calibration, task code T _ R4;
(5) a nadir main plane, a task code number T _ Z1;
(6) scaling the day by day and the day by the aid of the heaven and earth bottom main plane and a Z axis, and marking a task code T _ Z2;
(7) scaling the day by day and the X axis of the nadir main plane, and carrying out task code T _ Z3;
(8) the nadir principal plane + monthly calibration, task code T _ Z4;
(9) a nadir non-principal plane, a task code number T _ N1;
(10) the nadir non-principal plane + monthly calibration, task code T _ N2;
(11) target + gaze, task code T _ O1;
(12) target + region, task code T _ O2.
Further, the constraint conditions of the task sequence checking module include:
if 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);
if 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);
if 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);
wherein T _ N1= T _ Zj (j =1,2,3, 4);
wherein T _ R2, T _ Z2, are present at most once a day;
wherein T _ R3, T _ Z3, are provided at most once a month;
wherein CO2 has an internal scale 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 current day of the mission plan, i =2,3, …, Num, and T represents the current day.
Further, the task sequence planning of the task sequence generating module specifically includes:
firstly, judging whether a target observation requirement and an application track of target observation exist, and configuring a task of a selected track as a target observation T _ Oj (j =1, 2);
then, the first track task is scheduled to T _ Zj (j =1,2,3, 4);
secondly, according to task planning constraints, task configuration is carried out on the tasks of the rest tracks track by track, and the specific constraints correspond to the task sequence checking module;
finally, a track is selected from among the tracks assigned to task T _ Rj (j =1,2,3,4) or T _ Zj (j =1,2,3,4) for intra-CO 2 calibration.
A method of carbon satellite mission planning, the method comprising the steps of:
s1: the observation tasks of the carbon satellites are effectively arranged and combined to generate an effective task sequence, and effective combination of various observation tasks is realized;
s2: according to the observation task requirements and the task planning constraints, combining the parameter data file and the specific file, planning the task sequences of all the orbits in one day according to the carbon satellite task planning method, checking the task sequences, generating a task sequence file after checking, and sending the task sequence file to a pointing sequence generation system by using a network for the use of the satellite.
Further, the S1 includes the following steps:
the S1.1 carbon satellite observation tasks comprise sky bottom main plane observation, flare observation, sky bottom non-main plane observation, CO2 internal calibration, target observation, hot spot area observation, Z-axis sun-to-day calibration, X-axis sun-to-day calibration and moon calibration, and the observation tasks are effectively arranged and combined to generate an effective task sequence.
Further, the S2 includes the following steps:
s2.1: carrying out parameter configuration on target observation, daily calibration, monthly calibration and duty observation according to observation requirements, and configuring the rotation angle of the directional mirror according to the angle requirement of the directional mirror in each directional mode;
s2.2: the system automatically acquires a track data file, an illumination characteristic file and a target observation characteristic file from a designated position at regular time every day;
s2.3: the task sequence planning automatically calculates a target observable track according to the parameter setting and the acquired data file for the user to select;
s2.4: after determining a target observation task, a user autonomously selects a corresponding track to carry out target observation, and simultaneously carries out task sequence planning on other tracks on the same day according to task planning constraints;
s2.5: configuring the calibration tasks in the CO2 into corresponding task sequences to complete task sequence planning;
s2.6: after the task sequence planning is finished, the system automatically checks and feeds back the checking result to the user;
s2.7: and after the verification is passed, automatically sending the planned task sequence to a pointing sequence generation system, and if the verification is not passed, returning to target observation according to abnormal information to re-plan the task sequence.
Further, the S1.1 comprises the steps of:
based on the CO2 internal calibration of once a day, the observation is carried out through any one of the nadir main plane observation or flare observation tracks according to the observation requirement and the satellite energy limitation.
The invention has the beneficial effects that: in view of the fact that a planning method special for carbon satellite observation tasks does not exist in the prior art, due to the fact that carbon satellite observation requirements are various and complex and various observation modes designed for carbon satellites are aimed at, working modes of the carbon satellites are edited into effective task sequences, observation requirements and calibration requirements of the carbon satellites are met, carbon satellite observation data are effective, calibration accuracy of the carbon satellite observation data is improved, task planning of the carbon satellites is achieved, and the generated task sequences are automatically sent to a pointing sequence generation system through a network and are used by the carbon satellites.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings 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 invention, and it is obvious for those skilled in the art to obtain other drawings without creative efforts.
FIG. 1 is a block diagram of a system and method for carbon satellite mission planning according to an embodiment of the present invention;
fig. 2 is a block flow diagram of a system and method for carbon satellite mission planning according to an embodiment of the invention.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments that can be derived by one of ordinary skill in the art from the embodiments given herein are intended to be within the scope of the present invention.
As shown in fig. 1-2, a system and a method for carbon satellite mission planning according to an embodiment of the present invention includes:
the system comprises a parameter setting module, a data loading module and a task planning module, wherein the parameter setting module is used for configuring various parameters required by target observation, daily calibration, monthly calibration, a pointing mirror and a flare observation task, and the data loading module is used for loading a track data file, an illumination characteristic file and a target observation characteristic file required by task planning;
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 because the carbon satellite has multiple observation tasks and complex pointing modes and executes switching among different points and tasks and because the energy, storage capacity, attitude and other limitations exist among each other, determines the task sequence of the satellite in the orbit according to the main carbon observation task of the satellite in the orbit and the main pointing mode, timely selects the orbit to execute the calibration task in the carbon load according to the requirement and condition, and plans the task sequence of all the orbits in one day according to the requirement and the task planning constraint of the observation task by combining the parameters provided by the parameter setting module and the file provided by the data loading module according to the requirement and the task planning constraint of the carbon satellite, wherein the task sequence executed in one orbit comprises the following steps:
(1) flare, task code T _ R1;
(2) the flare + Z axis is calibrated to the day, and the task code is T _ R2;
(3) flare + X-axis daily calibration, task code T _ R3;
(4) flare + monthly calibration, task code T _ R4;
(5) a nadir main plane, a task code number T _ Z1;
(6) scaling the day by day and the day by the aid of the heaven and earth bottom main plane and a Z axis, and marking a task code T _ Z2;
(7) scaling the day by day and the X axis of the nadir main plane, and carrying out task code T _ Z3;
(8) the nadir principal plane + monthly calibration, task code T _ Z4;
(9) a nadir non-principal plane, a task code number T _ N1;
(10) the nadir non-principal plane + monthly calibration, task code T _ N2;
(11) target + gaze, task code T _ O1;
(12) target + region, task code T _ O2.
In a particular embodiment of the present invention,
the task sequence checking module is used for checking the task sequence planned by the task sequence planning module by task planning constraint to ensure that the task sequence meets constraint conditions and is used for:
if 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);
if 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);
if 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);
wherein T _ N1= T _ Zj (j =1,2,3, 4);
wherein T _ R2, T _ Z2, are present at most once a day;
wherein T _ R3, T _ Z3, are provided at most once a month;
wherein CO2 has an internal scale 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);
wherein Num represents the total number of orbits of the carbon satellites on the current day of the mission planning, i =2,3, …, Num, and T represents the current day;
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, the task sequence generation module gives an alarm and is used for:
firstly, judging whether a target observation requirement and an application track of target observation exist, and configuring a task of a selected track as a target observation T _ Oj (j =1, 2);
then, the first track task is scheduled to T _ Zj (j =1,2,3, 4);
secondly, according to task planning constraints, task configuration is carried out on the tasks of the rest tracks track by track, and the specific constraints correspond to the task sequence checking module;
finally, a track is selected from among the tracks assigned to task T _ Rj (j =1,2,3,4) or T _ Zj (j =1,2,3,4) for intra-CO 2 calibration.
A method of carbon satellite mission planning, the method comprising the steps of:
s1: the carbon satellite observation tasks comprise sky bottom main plane observation, flare observation, sky bottom non-main plane observation, CO2 internal calibration, target observation, hot spot area observation, Z-axis daily calibration, X-axis daily calibration and monthly calibration and are used for observing the effective arrangement combination of the tasks and generating an effective task sequence, wherein the CO2 internal calibration is performed once a day and is limited by observation requirements and on-satellite energy sources, and the task is performed through optional one of sky bottom main plane observation or flare observation orbits;
s2: carbon satellite task planning, according to observation task requirements and task planning constraints, combining parameter files and specific files, planning task sequences of all orbits in one day according to a carbon satellite task planning method, verifying the task sequences, generating task sequence files after verification, and sending the task sequence files to a pointing sequence generation system by using a network for the use of a satellite, further comprising:
s2.1: carrying out parameter configuration on target observation, daily calibration, monthly calibration and duty observation according to observation requirements, and configuring the rotation angle of the directional mirror according to the angle requirement of the directional mirror in each directional mode;
s2.2: the system automatically acquires a track data file, an illumination characteristic file and a target observation characteristic file from a designated position at regular time every day;
s2.3: the task sequence planning automatically calculates a target observable track according to the parameter setting and the acquired data file for the user to select;
s2.4: after determining a target observation task, a user autonomously selects a corresponding track to carry out target observation, and simultaneously carries out task sequence planning on other tracks on the same day according to task planning constraints;
s2.5: configuring the calibration tasks in the CO2 into corresponding task sequences to complete task sequence planning;
s2.6: after the task sequence planning is finished, the system automatically checks and feeds back the checking result to the user;
s2.7: and after the verification is passed, automatically sending the planned task sequence to a pointing sequence generation system, and if the verification is not passed, returning to target observation according to abnormal information to re-plan the task sequence.
In a specific embodiment of the present invention, the S2.4 task sequence planning includes the following steps:
s2.4.1 flare, task code T _ R1;
s2.4.2 flare + Z axis day-to-day calibration, task code T _ R2;
s2.4.3 flare + X-axis daily calibration, task code T _ R3;
s2.4.4 flare + monthly calibration, task code T _ R4;
s2.4.5 nadir main plane, task code T _ Z1;
s2.4.6 scaling day by day with the main plane at the bottom of the day and the Z axis, and a task code T _ Z2;
s2.4.7 scaling day by day with the main plane of the bottom of the day + X axis, and task code T _ Z3;
s2.4.8 nadir principal plane + monthly calibration, task code T _ Z4;
s2.4.9 nadir non-principal plane, task code T _ N1;
s2.4.10 nadir non-principal plane + monthly calibration, task code T _ N2;
s2.4.11 target + gaze, task code T _ O1;
s2.4.12 target + region, task code number T _ O2.
In an embodiment of the present invention, the S2.6 automatic verification includes the following steps:
s2.6.1, if 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, if 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, if 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)；
S2.6.5T _ R2, T _ Z2, at most once a day;
S2.6.6T _ R3, T _ Z3, at most once a month;
s2.6.7 CO2 has an internal standard 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 current day of the mission plan, i =2,3, …, Num, and T represents the current day.
In a specific embodiment of the present invention, the S2.7 comprises the following steps:
s2.7.1, judging whether there is a target observation requirement and a target observation application track, and configuring the task of the selected track as a target observation T _ Oj (j =1, 2);
s2.7.2 first track task schedule is T _ Zj (j =1,2,3, 4);
s2.7.3, according to the task planning constraint, carrying out task configuration on the tasks of the rest tracks track by track, wherein the specific constraint corresponds to the task sequence check module;
s2.7.4 select a track from the tracks assigned by the task as T _ Rj (j =1,2,3,4) or T _ Zj (j =1,2,3,4) for intra CO2 calibration.
In order to facilitate understanding of the above-described technical aspects of the present invention, the above-described technical aspects of the present invention will be described in detail below in terms of specific usage.
When the system and the method for planning the carbon satellite tasks are used specifically, the carbon satellite observation tasks effectively arrange and combine the observation tasks of the carbon satellites and generate an effective task sequence, and the effective combination of various observation tasks is realized; the carbon satellite mission planning, according to the observation mission requirement and the mission planning constraint, in combination with the parameter file and the specific file, draws out the mission sequences of all orbits in one day according to the carbon satellite mission planning method, verifies the mission sequences, generates the mission sequence file after the verification, and sends the mission sequence file to the pointing sequence generation system by using the network for the satellite to use, further includes:
firstly, carrying out parameter configuration on target observation, daily calibration, monthly calibration and duty observation according to observation requirements, and configuring the rotation angle of the directional mirror according to the angle requirement of the directional mirror in each directional mode;
step two, the system automatically acquires the track data file, the illumination characteristic file and the target observation characteristic file from the designated position at regular time every day;
step three, the task sequence planning automatically calculates a target observable track according to parameter setting and the acquired data file for a user to select;
after determining a target observation task, the user autonomously selects a corresponding track to carry out target observation, and simultaneously carries out task sequence planning on other tracks on the same day according to task planning constraints;
step five, configuring the calibration tasks in the CO2 into corresponding task sequences to complete task sequence planning;
step six, after the task sequence planning is finished, the system automatically checks and feeds back the checking result to the user;
and step seven, after the verification is passed, automatically sending the planned task sequence to a pointing sequence generation system, and if the verification is not passed, returning to the target observation according to the abnormal information to re-plan the task sequence.
In summary, according to the technical scheme of the invention, due to the fact that the carbon satellite has various observation requirements, a complex and various observation modes are designed for the carbon satellite, and in order to effectively control various modes of the carbon satellite and ensure the observation requirements and the calibration requirements of the satellite, an effective carbon satellite task planning system and an effective carbon satellite task planning method are designed to achieve task planning of the carbon satellite.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents, improvements and the like that fall within the spirit and principle of the present invention are intended to be included therein.
Claims (10)
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, sun calibration, moon calibration, a directional 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 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 checking module is used for checking 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, or else, giving an alarm.
2. The system for carbon satellite mission planning of claim 1, wherein the mission sequence planning module plans the operation mode of the carbon satellite in units of each orbit according to mission characteristics, determines the mission sequence of the satellite in the orbit according to the main carbon observation mission of the satellite in the orbit and the main pointing mode, and selects an orbit to execute the calibration mission in the carbon load at the right moment according to needs and conditions.
3. The carbon satellite mission planning system of claim 1, wherein the mission sequence planning module plans the mission sequences of all orbits in a day based on the carbon satellite mission planning module according to the observation mission requirements and mission planning constraints in combination with the parameters provided by the parameter setting module and the files provided by the data loading module.
4. The carbon satellite mission planning system of claim 3, wherein the mission sequence of the mission sequence planning module specifically comprises:
(1) flare, task code T _ R1;
(2) the flare + Z axis is calibrated to the day, and the task code is T _ R2;
(3) flare + X-axis daily calibration, task code T _ R3;
(4) flare + monthly calibration, task code T _ R4;
(5) a nadir main plane, a task code number T _ Z1;
(6) scaling the day by day and the day by the aid of the heaven and earth bottom main plane and a Z axis, and marking a task code T _ Z2;
(7) scaling the day by day and the X axis of the nadir main plane, and carrying out task code T _ Z3;
(8) the nadir principal plane + monthly calibration, task code T _ Z4;
(9) a nadir non-principal plane, a task code number T _ N1;
(10) the nadir non-principal plane + monthly calibration, task code T _ N2;
(11) target + gaze, task code T _ O1;
(12) target + region, task code T _ O2.
5. The system of carbon satellite mission planning of claim 1, wherein the constraints of the mission sequence checking module include:
if 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);
if 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);
if 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);
wherein T _ N1= T _ Zj (j =1,2,3, 4);
wherein T _ R2, T _ Z2, are present at most once a day;
wherein T _ R3, T _ Z3, are provided at most once a month;
wherein CO2 has an internal scale 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 current day of the mission plan, i =2,3, …, Num, and T represents the current day.
6. The system for carbon satellite mission planning of claim 1, wherein the mission sequence planning of the mission sequence generation module specifically comprises:
firstly, judging whether a target observation requirement and an application track of target observation exist, and configuring a task of a selected track as a target observation T _ Oj (j =1, 2);
then, the first track task is scheduled to T _ Zj (j =1,2,3, 4);
secondly, according to task planning constraints, task configuration is carried out on the tasks of the rest tracks track by track, and the specific constraints correspond to the task sequence checking module;
finally, a track is selected from among the tracks assigned to task T _ Rj (j =1,2,3,4) or T _ Zj (j =1,2,3,4) for intra-CO 2 calibration.
7. A method of carbon satellite mission planning, the method comprising the steps of:
s1: the observation tasks of the carbon satellites are effectively arranged and combined to generate an effective task sequence, and effective combination of various observation tasks is realized;
s2: according to the observation task requirements and the task planning constraint, combining the parameters provided by the parameter setting module and the files provided by the data loading module, planning the task sequences of all the orbits in one day according to the carbon satellite task planning method, verifying the task sequences, generating a task sequence file after verification, and sending the task sequence file to a pointing sequence generation system by using a network for the use of the satellite.
8. The method for carbon satellite mission planning according to claim 7, wherein said S1 includes the steps of:
the S1.1 carbon satellite observation tasks comprise sky bottom main plane observation, flare observation, sky bottom non-main plane observation, CO2 internal calibration, target observation, hot spot area observation, Z-axis sun-to-day calibration, X-axis sun-to-day calibration and moon calibration, and the observation tasks are effectively arranged and combined to generate an effective task sequence.
9. The method for carbon satellite mission planning according to claim 7, wherein said S2 includes the steps of:
s2.1: carrying out parameter configuration on target observation, daily calibration, monthly calibration and duty observation according to observation requirements, and configuring the rotation angle of the directional mirror according to the angle requirement of the directional mirror in each directional mode;
s2.2: the system automatically acquires a track data file, an illumination characteristic file and a target observation characteristic file from a designated position at regular time every day;
s2.3: the task sequence planning automatically calculates a target observable track according to the parameter setting and the acquired data file for the user to select;
s2.4: after determining a target observation task, a user autonomously selects a corresponding track to carry out target observation, and simultaneously carries out task sequence planning on other tracks on the same day according to task planning constraints;
s2.5: configuring the calibration tasks in the CO2 into corresponding task sequences to complete task sequence planning;
s2.6: after the task sequence planning is finished, the system automatically checks and feeds back the checking result to the user;
s2.7: and after the verification is passed, automatically sending the planned task sequence to a pointing sequence generation system, and if the verification is not passed, returning to target observation according to abnormal information to re-plan the task sequence.
10. The method of carbon satellite mission planning according to claim 8, wherein said S1.1 comprises the steps of:
based on the CO2 internal calibration of once a day, the observation is carried out through any one of the nadir main plane observation or flare observation tracks according to the observation requirement and the satellite energy limitation.
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