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An energy constraint system and method for satellite planning tasks

A technology for restraining system and energy, applied in the field of satellite mission simulation, can solve problems such as inaccurate initial value, inability to quickly adjust tasks, inaccurate calculation results, etc., to achieve the effect of eliminating calculation errors and accurate energy energy constraint inspection

Active Publication Date: 2021-03-16
SHANGHAI ENG CENT FOR MICROSATELLITES
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  • Abstract
  • Description
  • Claims
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Problems solved by technology

[0006] The purpose of this application is to provide an energy constraint system for satellite planning tasks that performs energy constraint checks on planning tasks during the entire satellite operation period, thereby solving the above-mentioned technical problems in the prior art
This application overcomes the shortcomings of inaccurate initial values ​​caused by discontinuous energy data in the existing energy constraint calculation method, no adjustment suggestions are given when the energy constraint fails, resulting in inability to quickly adjust the task, and inaccurate calculation results due to uncorrected calculation errors. An energy database-centric energy constraint checking system is proposed

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  • An energy constraint system and method for satellite planning tasks
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Embodiment Construction

[0039] The technical solutions of the present application will be clearly and completely described below in conjunction with the accompanying drawings and the embodiments of the present application.

[0040] In the first aspect, this application proposes an energy constraint system for satellite planning tasks. The system is centered on the energy database, and consists of five tasks: energy constraint calculation during the mission period, task adjustment, energy calculation during the non-mission period, telemetry correction, and database maintenance. consists of modules. Among them, the mission-period energy constraint calculation module is an existing energy constraint system, and the other four modules are methods proposed by this application. Through the above five modules, the energy database can calculate and accurately record the energy consumption of the satellite's entire operation cycle, and finally achieve the purpose of energy constraints for planning tasks.

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Abstract

The present application relates to an energy constraint system for satellite planning tasks, which performs energy constraint checks on the planning tasks during the entire satellite operation period. The system of this application uses the energy database to record the energy data of the entire operation cycle of the satellite, which can accurately obtain the initial energy value, adjust the task according to the task priority when the energy constraint check fails, and introduce real telemetry data to correct the energy data Elimination of calculation errors enables accurate energy constraint checks throughout the satellite's entire operating cycle. The present application also provides a method for performing energy constraints on satellites using the energy constraint system for satellite planning tasks as described herein.

Description

technical field [0001] This application relates to the technical field of satellite mission simulation, and specifically relates to an energy constraint system and method for satellite planning tasks, which are applied to earth observation satellites that require mission planning, and perform energy constraint checks on planned tasks during the entire satellite operation period. Background technique [0002] Earth observation satellites carry space-borne sensors such as visible light, electronic reconnaissance, and synthetic aperture radar to obtain information such as images and signals of ground targets, and transmit this information back to the ground station for analysis and use. Due to the high cost of satellites, satellite resources are particularly valuable. In order to make full use of satellite-ground resources and maximize the effectiveness of satellites, it is necessary to plan missions for satellites to maximize the use of satellite resources. In the process of m...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06Q10/06
CPCG06Q10/06375B64G1/10
Inventor 李立朱野赵灵峰张越陈雨张晓杰
Owner SHANGHAI ENG CENT FOR MICROSATELLITES
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