Negative-imaginary-based spacecraft attitude tracking control using modified Rodrigues parameters

Xiaoyu Lang*, Xiangdong Liu, Zhen Chen

*此作品的通讯作者

科研成果: 期刊稿件文章同行评审

摘要

This paper investigates a counter-clock-wise input-output map about spacecraft attitude dynamics and kinematics using Modified Rodrigues Parameters. A gyro-free attitude control scheme is established by constructing a negative imaginary system for spacecraft attitude stabilization. Attitude tracking control scheme is also explored where the negative-imaginary-based controller has no need on the angular velocity measurements. Numerical simulations are presented to show the effectiveness of the proposed attitude control scheme.

源语言英语
文章编号109057
期刊Aerospace Science and Technology
147
DOI
出版状态已出版 - 4月 2024

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