Release Time:2019-03-11  Hits:

Indexed by: Conference Paper

Date of Publication: 2011-12-12

Included Journals: Scopus、CPCI-S、EI

Page Number: 8304-8308

Abstract: The problem of spacecraft relative position holding with limited thrust and thruster nonlinearity is investigated in this paper. The relative dynamic model with sampled-data measurement is established based on the Clohessy-Wiltshire (C-W) equations. Thruster nonlinearity and limited thrust constraint are taken into consideration. Then, the relative position holding problem is regarded as a sampled-data output tracking control problem. Based on Lyapunov stabilization theory, the sampled-data controller is designed by solving a convex optimization problem. Simulations show the effectiveness of the proposed method.