An Autonomous Request Orbit Service System for Microsatellites

Abstract

A micro-satellite independent request orbit service system, which includes a ground measurement and control system, on-board management and control application software, and satellite-ground data interaction interface; the ground measurement and control system, including a measurement and control center and a measurement and control station, is used for remote control command injection and telemetry data reception processing and precise orbit determination; the spaceborne management and control application software includes an autonomous orbit determination module, a high-precision orbit forecast module, and a task scheduling management module; the satellite-ground data interaction interface is used to realize the format agreement of the satellite-ground uplink data and downlink data. The purpose of the present invention is to provide a micro-satellite autonomous control technology that can maintain orbit prediction results equivalent to the accuracy of orbit calculations on the ground on the satellite, so as to solve the problem that the existing technology can only meet the requirements of satellites in general micro-satellite orbit prediction tasks. The medium precision requirements of the position are difficult to meet the technical problems of high precision requirements for satellite payload applications such as autonomous mission planning.

Description

technical field [0001] The invention belongs to the field of aerospace technology, in particular to a micro-satellite autonomous control technology, and in particular to a micro-satellite autonomous request orbit service system. Background technique [0002] With the development of aerospace technology, especially the widespread application of microsatellite technology in recent years, the computing and storage capabilities of onboard computers have been continuously enhanced, and the cost of development and launch of microsatellites has been significantly reduced. Improving the autonomous operation capability of microsatellites is of great significance for reducing the overhead of measurement and control resources, reducing the pressure on ground management and control, and providing orbital services to other spaceborne applications. [0003] In order to realize the autonomous control of microsatellites, the required orbital service functions mainly include real-time orbit ...

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide a micro-satellite autonomous control technology that can maintain orbit prediction results equivalent to the accuracy of orbit calculations on the ground on the satellite, so as to solve the problem that the existing technology can only meet the requirements of satellites in general micro-satellite orbit prediction tasks. The medium precision requirements of the position make it difficult to meet the technical problems of high precision requirements for satellite payload applications such as autonomous mission planning

Images