考虑控制饱和的卫星姿态控制器设计

Abstract

Abstract: The problem addressed is the modified rodrigues parameter (MRP) based attitude control for rigid spacecraft subject to control input constraints.First a full state feedback controller is proposed, and the Lyapunov theory is employed to prove the global asymptotic stability of the zero equilibrium points of the closed loop system.Then an output feedback control scheme that is dependent on MRP is designed without angular velocity measurements.On the other hand, by introducing ahyperbolic tangent saturation function into the control scheme, it can be concluded that the control input saturation problem can be effectively restrained so long as the control parameters are selected to satisfy a specific inequality.Simulation results demonstrate the effectiveness and feasibility of the proposed control scheme.

Key words:

font-size:10.5pt, font-family:Calibri, sans-serif, "> color:windowtext, attitude control')">">attitude control, output feedback control, control saturation, MRP,

font-size:10.5pt, font-family:Calibri, sans-serif, "> ')">"> ,

CLC Number:

V442

LV Jianting, MA Guangfu, GAO Dai.

Satellite Attitude Controller Design Subject to Input Saturation [J].Aerospace Contrd and Application, 2008, 34(2): 33-36.

0
/ Save 0 / Recommend attitude control;output feedback control;control saturation;MRP;

”. Please open it by linking:http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/abstract/abstract9394.shtml" name="neirong"> attitude control;output feedback control;control saturation;MRP;

">

Add to citation manager EndNote|Reference Manager|ProCite|BibTeX|RefWorks

URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/

http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2008/V34/I2/33

References

Metrics

Viewed

Full text

156

HTML			PDF

Just accepted	Online first	Issue	Just accepted	Online first	Issue
0	0	0	0	0	156

From	Others	local

Times	41	115
Rate	26%	74%

Abstract

Just accepted	Online first	Issue

0	0	38

	From	Others

	Times	38
	Rate	100%

Cited

Web of Science	Crossref	ScienceDirect	Satellite Attitude Controller Design Subject to Input Saturation " target="_blank">Search for Citations in Google Scholar >>


This page requires you have already subscribed to WoS.

Shared

[1]	HU Qi, CHEN Jian, LI Yong. Numerical Simulation for Reorientation of Propellant in a Vane Tank under Microgravity [J]. Aerospace Contrd and Application, 2009, 35(6): 54-57.
[2]	ZHANG Jinfeng, SUN Chengqi, CAI Wei. Monocular Vision-Based Relative Position and Attitude Measurement Algorithm for Non-Cooperative Spacecrafts [J]. Aerospace Contrd and Application, 2009, 35(6): 50-53.
[3]	CHEN Changqing, XIE Yonghcun. Quadratic-Based Computation of Four-Impulse Optimal Rendezvous between Near Circular Orbits [J]. Aerospace Contrd and Application, 2009, 35(6): 45-49.
[4]	XU Jingyu, GAO Yijun. Sun Sensor-Based Orbit Position Estimating Method for GEO Satellites [J]. Aerospace Contrd and Application, 2009, 35(6): 41-44.
[5]	SHEN BenjianLIU HaiboJIA HuiYANG JIankun. CCD Chip’s Temperature Effect on Position Accuracy of Star Sensor [J]. Aerospace Contrd and Application, 2009, 35(6): 36-40.
[6]	LI Gming, YAO Yu. Design of Space Rendezvous and Docking Transverse Linear Movement Simulator Control System Based on H∞ Theory [J]. Aerospace Contrd and Application, 2009, 35(6): 30-35.
[7]	LIANG Dong, , WANG Pengji, , LIU Liangdong . A LIDAR-Based Autonomous Landing Site Selection Method for Pinpoint Lunar Soft Landing [J]. Aerospace Contrd and Application, 2009, 35(6): 24-29.
[8]	GONG Dezhu, WU Yanpeng, LU Xin. An Attempt at Improving Dynamic Performance of Star Tracker by Motion Compensation [J]. Aerospace Contrd and Application, 2009, 35(6): 19-23.
[9]	YUAN Li, CHENG Ming . Deep Space Exploration Mission-Oriented Flight Control Simulation and Support System#br# [J]. Aerospace Contrd and Application, 2009, 35(6): 13-18.
[10]	ZHANG Jun, , HU Haixia, . Dynamics Modeling and Simulation Verification for Space Robot [J]. Aerospace Contrd and Application, 2009, 35(6): 6-12.
[11]	LI Guo. A Survey of GNC Critical Techniques for Development of China Spacecrafts in the Future [J]. Aerospace Contrd and Application, 2009, 35(6): 1-5.
[12]	YANG Mengfei JIA Yang CHEN Jianxin. Research on System Design of Lunar Rover [J]. Aerospace Contrd and Application, 2008, 34(3): 3-6.
[13]	SHEN Shaopin, WU Hongxin, . A Method of Intelligent Adaptive Control for Spacecraft [J]. Aerospace Contrd and Application, 2008, 34(3): 7-11.
[14]	ZOU Dali, YANG Lei, QU Guangji. Research on the Attitude Control of Active Suspension Rov [J]. Aerospace Contrd and Application, 2008, 34(3): 12-16.
[15]	LI Ji.. Fault Diagnosis Method Based on a Decentralized Predictive Filter [J]. Aerospace Contrd and Application, 2008, 34(3): 17-22.

Satellite Attitude Controller Design Subject to Input Saturation

PDF (PC)

Like

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Metrics

Comments

Recommended 0