Adaptive output feedback control of spacecraft with flexible appendages by modeling error compensation

Acta Astronautica

Volumn 54, Issue 4, 2004, Pages 229-243

  Singh, Sahjendra N ^a   Zhang, Rong ^a  

^a UNIVERSITY OF NEVADA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; DEFORMATION; DYNAMICS; FEEDBACK CONTROL; LYAPUNOV METHODS; REMOTE SENSING; TRAJECTORIES; VIBRATIONS (MECHANICAL);

LYAPUNOV STABILITY THEORY; VIBRATION SUPPRESSION;

SPACECRAFT;

EID: 0344740641     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0094-5765(03)00030-4     Document Type: Article

References (34)

1. A.J. Miller, G.L. Gray, A.P. Mazzoleni, Nonlinear spacecraft dynamics with flexible appendage, damping, and moving internal submasses, Journal of Guidance, Control, and Dynamics 42(3) (2001) 605-615.
2. T. Nagata, V.J. Modi, H. Matsuo, Dynamics and control of flexible multibody systems part I: general formulation with an order N forward dynamics, Acta Astronautica 49(11) (2001) 581-594.
3. T. Nagata, V.J. Modi, H. Matsuo, Dynamics and control of flexible multibody systems part II: simulation code and parametric studies with nonlinear control, Acta Astronautica 49(11) (2001) 595-610.
4. D.C. Hyland, J.L. Junkins, R.W. Longman, Active control technology for space structures, Journal of Guidance, Control, and Dynamics 16 (1993) 801-821.
5. J. Ben-Asher, J.A. Burns, E.M. Cliff, Time optimal slewing of flexible spacecraft, Journal of Guidance, Control, and Dynamics 15 (1992) 360-367.
6. G. Singh, P.T. Kabamba, N.H. McClamroch, Bang-bang control of flexible spacecraft Slewing maneuvers: guaranteed terminal pointing accuracy, Journal of Guidance, Control, and Dynamics 13 (1990) 376-379.
7. R.M. Byers, S.R. Vadali, J.L. Junkins, Near-minimum-time open-loop slewing of flexible vehicles, Journal of Guidance, Control, and Dynamics 13 (1990) 57-65.
8. J.D. Turner, H.M. Chun, Optimal distributed control of a flexible spacecraft during a large-angle maneuver, Journal of Guidance and Control (1984) 257-264.
9. J.L. Junkins, Z. Rahman, H. Bang, Near minimum-time maneuvers of flexible vehicles: analytical and experimental results, Journal of Guidance, Control, and Dynamics 14 (1991) 406-415.
10. A. Grewal, V.J. Modi, Robust attitude and vibration control of the space station, Acta Astronautica 38(3) (1996) 139-160.
11. A.A. Bolonkin, N.S. Khot, Optimal bounded control design for vibration suppression, Acta Astronautica 38(10) (1996) 803-813.
12. A.K. Banerjee, N. Padereiro, Vibration reduction for flexible spacecraft following momentum dumping with/without slewing, Journal of Guidance, Control, and Dynamics 24(3) (2001) 417-427.
13. D. Gorinevsky, G. Vukovich, Nonlinear input shaping control of flexible spacecraft reorientation maneuver, Journal of Guidance, Control, and Dynamics 21(2) (1998) 264-270.
14. E.H. Teague, J.P. How, B.W. Parkinson, Control of flexible structure using GPS: methods and experimental results, Journal of Guidance, Control, and Dynamics 21(5) (1998) 673-683.
15. P.S. Goel, P.K. Maharana, An active damping technique for satellites with flexible appendages, Acta Astronautica 36(5) (1995) 239-250.
16. G. Song, B.N. Agrawal, Vibration suppression of flexible spacecraft during attitude control, Acta Astronautica 49(2) (2001) 73-84.
17. S.Di. Gennaro, Active vibration suppression in flexible spacecraft attitude tracking, Journal of Guidance, Control, and Dynamics 21(3) (1998) 400-408.
18. H-H. Zhang, H. Matsuo, Y. Morita, H. Yamakawa, Stabilization of a deployable flexible structure, Acta Astronautica 43(7-8) (1998) 369-376.
19. R.D. Quinn, L. Meirovitch, Maneuvering and vibration control of SCOLE, Journal of Guidance, Control, and Dynamics 11 (1988) 542-553.
20. J.L. Junkins, H. Bang, Maneuver and vibration control of hybrid coordinate systems using Lyapunov stability theory, Journal of Guidance, Control, and Dynamics 16 (1993) 668-676.
21. A. Isidori, Nonlinear Control Systems, Springer, New York, 1989, pp. 145-173.
22. J.E. Slotine, W. Li, Applied Nonlinear Control, Prentice-Hall, Englewood Cliffs, NJ, 1991.
23. S.N. Singh, Robust nonlinear attitude control of flexible spacecraft, IEEE Transactions on Aerospace and Electronic Systems 23 (1987) 380-387.
24. S. Monaco, S. Stornelli, A nonlinear attitude control law for a satellite with flexible appendages, Proceedings of the 24th Conference on Decision and Control, 1985, pp. 1654-1659.
25. F. Karray, A. Grewal, M. Glaum, V. Modi, Stiffening control of a class of nonlinear affine systems, IEEE Transactions on Aerospace and Electronic Systems 33(2) (1997) 473-484.
26. A. Iyer, S.N. Singh, Variable structure slewing control and vibration damping of flexible spacecraft, Acta Astronautica 25 (1991) 1-9.
27. Y. Zeng, A. Araujo, S.N. Singh, Output feedback variable structure adaptive control of a flexible spacecraft, Acta Astronautica 44 (1999) 11-22.
28. J. Alvarez-Ramirez, Adaptive control of feedback linearizable systems: a modeling error compensation approach, International Journal of Robust and Nonlinear Control 9 (1999) 361-377.
29. F. Esfandiari, H.K. Khalil, Output feedback stabilization of fully linearizable systems, International Journal of Control 56(5) (1992) 1007-1037.
30. H.K. Khalil, Adaptive output feedback control of nonlinear systems represented by input-output models, IEEE Transactions on Automatic Control 41(2) (1996) 177-188.
31. H.K. Khalil, F. Esfandiari, Semiglobal stabilization of a class of nonlinear systems using output feedback, IEEE Transactions on Automatic Control 38(9) (1993) 1412-1415.
32. T. Kailath, Linear Systems, Prentice-Hall, Englewood Cliffs, NJ, 1980.
33. H.K. Khalil, Nonlinear Systems, Macmillan Publishing Company, NY, 1992.
34. M. Vidyasagar, Nonlinear Systems Analysis, Prentice-Hall, Englewood Cliffs, NJ, 1993.