Title :
Attitude control of a satellite using the SDRE method
Author :
Parrish, David K. ; Ridgely, D. Brett
Author_Institution :
Air Force Inst. of Technol., Wright-Patterson AFB, OH, USA
Abstract :
Examines the use of nonlinear regulation for attitude control of a satellite controlled by internal momentum rotors. Specifically, the nonlinear method using the state dependent Riccati equation (SDRE) developed by Cloutier, D´Souza, and Mracek (1996) is applied and examined under numerical simulations
Keywords :
Riccati equations; artificial satellites; attitude control; linear quadratic control; nonlinear control systems; attitude control; internal momentum rotors; nonlinear regulation; state dependent Riccati equation; Aerodynamics; Nonlinear equations; Optimal control; Quaternions; Riccati equations; Satellites; Space technology; Stability; State-space methods; Tensile stress;
Conference_Titel :
American Control Conference, 1997. Proceedings of the 1997
Conference_Location :
Albuquerque, NM
Print_ISBN :
0-7803-3832-4
DOI :
10.1109/ACC.1997.609665
