Attitude Control of Spacecraft by State Dependent Riccati Equation and Power Series Expansion of Riccati Methods

M. Navabi; M. Tavana; H.R. Mirzaei

Volume 7, Issue 4 , January 2015, , Pages 39-49

Abstract
  Attitude control of spacecraft in order to nonlinear and high order dynamics is fundamental and challenging issue. With respect to these nonlinearities, linear control theories are not suitable choices and spacecraft may be unstable or lose performance. In this paper, State Dependent Riccati Equation ...  Read More