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 |
卷 | 147 |
DOI | |
出版状态 | 已出版 - 4月 2024 |