Design of satellite control system using optimal nonlinear theory

Mechanics Based Design of Structures and Machines

Volumn 34, Issue 4, 2006, Pages 351-364

  De Souza, Luiz Carlos Gadelha ^a  

^a INSTITUTO NACIONAL DE PESQUISAS ESPACIAIS   (Brazil)

Author keywords

Nonlinear theory; Satellite attitude control

Indexed keywords

EQUATIONS OF MOTION; LINEAR EQUATIONS; NONLINEAR CONTROL SYSTEMS; NONLINEAR SYSTEMS; PRODUCT DESIGN;

ATTITUDE CONTROL SYSTEMS (ACS); LINEAR QUADRATIC REGULATOR (LQR) THEORY; NONLINEAR CONTROL THEORY; SATELLITE ATTITUDE CONTROL;

SATELLITES;

EID: 33845395585     PISSN: 15397734     EISSN: 15397742     Source Type: Journal    
DOI: 10.1080/15397730601044853     Document Type: Conference Paper

References (13)

1. Al'Brekht, E. G. (1962). On the optimal stabilization of non-linear systems. Journal of Applied Mathematics Mechanics 25(5):1254-1266.
2. Chen, Y., Manousiouthkis, V., Edgar, T. (2006). Globally optimal nonlinear feedback: application to nonisothermal CSTR control. Chemical Engineering Communications 193(2):233-245(13).
3. Dabbous, T. E., Ahmed, N. V. (1981). Nonlinear feedback regulation of satellite angular moments. IEEE Transaction on Aerospace and Electronic Systems 8(1):2-10.
4. Fenili, A., Souza, L. C. G. (2004). Control of a nonlinear slewing flexible beam. In: Proc. of 21st International Congress of Theoretical and Applied Mechanics. Warsaw, Poland, August 15-21.
5. Lukes, D. L. (1969). Optimal regulation of nonlinear dynamical systems. SIAM Journal 7(1):75-100.
6. Kalman, R. E. (1960). Contributions to the theory of optimal control. Mexican Mathematics Society Bulletin 2(5):102-119.
7. Kailath, T. (1980). Linear Systems. New York: Prentice-Hall.
8. Parrish, D. K., Ridgely, D. B. (1997). Attitude control of a satellite using the SDRE method. In: Proc. American Control Conference. Vol. 2. Albuquerque, NM, pp. 942-946.
9. Silva, A. R., Schäfer, B., Souza, L. C. G., Fonseca, R. A. (2000). Integrated linear and non-linear parameters identification for space robot dynamics. In: Proc. of 51st International Astronautical Congress. Rio de Janeiro, Brazil.
10. Souza, L. C. G. (1987). Application of a extension of the linear quadratic regulator method to satellite attitude control. Master Theses. National Institute for Space Research - INPE, São José dos Campos-SP. Brasil.
11. Vargas, R., Souza, L. C. G., Kuga, H. K. (2004). Application of the Kalman filter to estimate elastic parameters in order to improve controller performance. In: Tadeu, A., Atluri, S. N., eds. Proc. of the International Conference on Computational & Experimental Engineering & Sciences 26-29 July, Madeira, Portugal.
12. Willemstein, A. P. (1977). Optimal regulation of nonlinear dynamical systems on a finite interval. SIAM Journal 15(6):1050-1069.
13. Zheng, J. (2006). Comparation of two linearization methods for optimal attitude maneuver of a nonlinear flexible spacecraft. Journal of Mathematical Control and Information 23:127-136.