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2022 | OriginalPaper | Buchkapitel

A Differential Flat Approach for Attitude Manoeuver Control of Agile Satellite

verfasst von : Deting Li, Yikang He, Shuyu Lin, Miao Li, Kang Shi

Erschienen in: Proceedings of the 7th China High Resolution Earth Observation Conference (CHREOC 2020)

Verlag: Springer Nature Singapore

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Abstract

This pater introduces a kind of control method for agile satellites which use SGCMG as actuators. Considering the SGCMG’s singularities, an attitude trajectory planning method is designed based on the differential flatness theory firstly. This method considers the singularity features and the influence of gravity gradient torque. A sliding mode tracking controller is proposed based on the Modified Rodrigues parameters. Result of simulation shows that the SGCMG undergoing large maneuver without singularity and the tracking error is less than 0.03°, the attitude deviation in the steady state is less than 1 × 10–5°.

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Metadaten
Titel
A Differential Flat Approach for Attitude Manoeuver Control of Agile Satellite
verfasst von
Deting Li
Yikang He
Shuyu Lin
Miao Li
Kang Shi
Copyright-Jahr
2022
Verlag
Springer Nature Singapore
DOI
https://doi.org/10.1007/978-981-16-5735-1_15

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