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

被引：1
作者：
Lang, Xiaoyu [1 ]
Liu, Xiangdong [1 ]
Chen, Zhen [1 ]
机构：
[1] Beijing Inst Technol, Sch Automat, Zhongguancun South St 5, Beijing 100081, Peoples R China
来源：
AEROSPACE SCIENCE AND TECHNOLOGY | 2024年 / 147卷
基金：
中国国家自然科学基金;
关键词：
Spacecraft attitude control; Modified Rodrigues parameters; Negative imaginary control; SYSTEMS;
D O I：
10.1016/j.ast.2024.109057
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
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.
引用
收藏
页数：7
相关论文
共 30 条
123