Robust Control of Spacecraft Formation Flying Using Optimal Sliding Mode

A. Imani; M. Bahrami

Volume 6, Issue 1 , April 2013, , Pages 69-75

Abstract
  In this paper, in order to control the relative motion for spacecraft formation flying, an optimal sliding mode controller is presented. This controller is designed based on the linearized equations of relative motion in circular orbit and applied to nonlinear system that is subjected to external disturbance. ...  Read More