Fully-Actuated System Approach Based Optimal Attitude Tracking Control of Rigid Spacecraft with Actuator Saturation

被引：10
|
作者：
Liu Gaoqi [1 ]
Zhang Kai [1 ]
Li Bin [1 ]
机构：
[1] Sichuan Univ, Sch Aeronaut & Astronaut, Chengdu 610065, Peoples R China
来源：
JOURNAL OF SYSTEMS SCIENCE & COMPLEXITY | 2022年 / 35卷 / 02期
基金：
中国国家自然科学基金;
关键词：
Full-actuated system approach; modified Rodrigues parameters; parameter optimization; spacecraft attitude tracking; STABILIZATION;
D O I：
10.1007/s11424-022-1515-8
中图分类号：
O1 [数学];
学科分类号：
0701 ; 070101 ;
摘要：
In this paper, a fully-actuated system approach (FASA) based control method is proposed for rigid spacecraft attitude tracking with actuator saturation. First, a second-order fully-actuated form of spacecraft attitude error model is established by modified Rodrigues parameters (MRPs). The unknown total disturbance caused by inertial uncertainty and external disturbance is estimated by using extended state observer, then an FASA based controller is developed. Further, a control parameterization method is adopted to optimize the parameter matrices of FASA based controller with the actuator saturation. Finally, a numerical example is carried out to validate the effectiveness of the proposed scheme.
引用
收藏
页码：688 / 702
页数：15
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