Aerospace Contrd and Application ›› 2008, Vol. 34 ›› Issue (3): 30-36.
Previous Articles Next Articles
Robust Control of Large Angle Maneuver for Multi-Body Spacecraft
Online:
Published:
Abstract: This paper investigates the robust control of large angle maneuver for the multi-body spacecraft with model uncertainties.A nonlinear dynamics model with uncertainties is considered.An approximate pseudo-linear system is developed by using the inverse system method,and two linear robust controllers are designed through the mixed sensitivity H∞ optimization and the p synthesis method,respectively.A PD controller is used to eliminate the singularity during the mixed sensitivity H∞ optimization.Numerical examples of the central body and antenna tracking different targets are given.The simulation results demonstrate that both controllers are robust stable,and the robust performance of the μ controller is better than that of the H∞ controller.
Key words: font-family:Calibri, sans-serif, multi-body spacecraft">multi-body spacecraftfont-family:宋体, ')">">, font-family:Calibri, sans-serif, H">Hfont-family:Arial, sans-serif, ∞ ')">">∞ , font-family:Calibri, sans-serif, control">controlfont-family:宋体, ')">">, font-family:Calibri, sans-serif, μ ">μ font-family:Calibri, sans-serif, synthesis">synthesisfont-family:宋体, ')">">, font-family:Calibri, sans-serif, large angle maneuver">large angle maneuver')">">
CLC Number:
YUAN Changqing, LI Junfeng, SHEN Ying, .
Robust Control of Large Angle Maneuver for Multi-Body Spacecraft [J].Aerospace Contrd and Application, 2008, 34(3): 30-36.
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/I3/30
Cited