The robust control of sun-earth L2 point formation flying

Author

Pan Xiong ; Jian, Chen ; Feng Wang ; Li, Shi ; Xibin Cao

Author_Institution

Res. Center of Satellite Technol., Harbin Inst. of Technol., Harbin, China

fYear

2012

fDate

18-20 July 2012

Firstpage

377

Lastpage

382

Abstract

A robust nonlinear controller is developed for the formation flying system. Using a nonlinear model directly, the Polynomial Eigenstructure Assignment approach is applied to complete controller design. The resulting controller can produce a closed-loop system with invariant performance over a wide range of conditions. Taking two sources of uncertainty, the robust D-stability is assessed by using the Finite Inclusion Theorem. The results show that the closed-loop system is fairly robust with respect to the uncertainties.

Keywords

Earth; Sun; aircraft control; closed loop systems; eigenstructure assignment; nonlinear control systems; polynomials; robust control; uncertain systems; Sun-Earth L₂ point formation flying system; closed-loop system; controller design; finite inclusion theorem; polynomial eigenstructure assignment approach; robust D-stability; robust nonlinear controller; spacecraft formation flying; uncertainties; Closed loop systems; Mathematical model; Nonlinear dynamical systems; Polynomials; Robustness; Uncertainty;

fLanguage

English

Publisher

ieee

Conference_Titel

Industrial Electronics and Applications (ICIEA), 2012 7th IEEE Conference on

Conference_Location

Singapore

Print_ISBN

978-1-4577-2118-2

Type

conf

DOI

10.1109/ICIEA.2012.6360756

Filename

6360756