Thruster Control for Micro-satellite Attitude and Hardware-in-the-loop Demonstration

被引：0

作者：

Hu Min ^{[1
]}

Zeng Guoqiang ^{[2
]}

Gao Yudong ^{[2
]}

机构：

[1] Acad Equipment, Postgrad Sch, Beijing, Peoples R China

[2] Natl Univ Defense Technol, Inst Aerosp & Mat Engn, Changsha, Peoples R China

来源：

2012 INTERNATIONAL CONFERENCE ON INDUSTRIAL CONTROL AND ELECTRONICS ENGINEERING (ICICEE) | 2012年

关键词：

micro-satellite; attitude control; phase-plane method; PWPF modulator; mono-axis air-bearing table; hardware-in-the-loop; SPACECRAFT;

D O I：

10.1109/ICICEE.2012.160

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

This paper investigates the thruster control problem for micro-satellite attitude. Firstly, the attitude dynamic and kinematics equations are introduced. Secondly, the phase plane optimal attitude control algorithms are put forward, and the Pulse-Width Pulse-Frequency (PWPF) modulator is also designed. Then, the hardware-in-the-loop simulation system based on the air-bearing table are introduced and established to validate the control algorithms. Finally, the simulations are carried out. The simulation results indicate that the proposed methods are effective and feasible, which can realize the high accuracy attitude control for micro-satellite.

引用

页码：588 / 591

页数：4

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