Investigation in to The Effect of Kinematic of The Space Craft Attitude Control Using Feedback Linearization Method

M. Navabi; M.R. Hosseini

Volume 11, Issue 1 , June 2018, , Pages 59-71

Abstract
  Using nonlinear control theories is common for the attitude control problem of spacecraft.Feedback linearization theory is a nonlinear control method which tries to transform nonlinear dynamics of system into linear.In this control theory, outputs choice will have a direct impact on the stability ...  Read More