Magnetic torque attitude control of a satellite using the state-dependent Riccati equation technique

Author:

Abdelrahman Mohammad,Chang Insu,Park Sang-Young

Publisher

Elsevier BV

Subject

Applied Mathematics,Mechanical Engineering,Mechanics of Materials

Reference36 articles.

1. E.B. Erdem, Analysis and real-time implementation of state-dependent Riccati equation controlled systems, Ph.D. Dissertation, University of Illinois at Urbana-Champaign, Illinois, 2001, pp. 5–35.

2. J.R. Cloutier, C.N. D'Souza, C.P. Mracek, Nonlinear regulation and nonlinear H∞ control via the state-dependent Riccati equation technique; Part 1, Theory; Part 2, Examples, in: Proceedings of the 1st International Conference on Nonlinear Problems in Aviation and Aerospace, Available through University Press, Embry-riddle Aeronautical University, Daytona Beach, FL, May 1996.

3. J.R. Cloutier, D.T. Stansbery, The capabilities and art of state-dependent Riccati equation-based design, in: Proceedings of the American Control Conference, Anchorage, Alaska, May 2002.

4. J.R. Cloutier, D.T. Stansbery, Nonlinear, hybrid bank-to-turn/skid-to-turn autopilot design, in: Proceedings of the Guidance, Navigation, and Control Conference, Montreal, Canada, August 2001.

5. J.R. Cloutier, P.H. Zipfel, Hypersonic guidance via the state-dependent Riccati equation control method, in: Proceedings of the IEEE Conference on Control Applications, Hawaii, August 1999.

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