Robust backstepping sliding mode attitude tracking and vibration damping of flexible spacecraft with actuator dynamics

Journal of Aerospace Engineering

Volumn 22, Issue 2, 2009, Pages 139-152

  Hu, Qinglei ^a,b   Cao, Jun ^a   Zhang, Yizhuo ^a  

^a NORTHEAST FORESTRY UNIVERSITY   (China)

^b North East Forest University   (China)

Author keywords

Control systems; Spacecraft; Vibration

Indexed keywords

ASYMPTOTIC ANALYSIS; ASYMPTOTIC STABILITY; ATTITUDE CONTROL; BACKSTEPPING; CONTROL SYSTEM ANALYSIS; DYNAMICS; FEEDBACK; FLIGHT DYNAMICS; NAVIGATION; PIEZOELECTRIC ACTUATORS; ROBUST CONTROL; SENSORS; SPATIAL VARIABLES CONTROL; STRAIN RATE; VIBRATORS; WHEELS;

ACTUATOR DYNAMICS; ADAPTIVE VERSIONS; ASYMPTOTIC CONVERGENCES; ATTITUDE CONTROL SYSTEMS; ATTITUDE CONTROLLERS; ATTITUDE MOTIONS; ATTITUDE TRACKING; ATTITUDE TRACKING CONTROLS; BACKSTEPPING TECHNIQUES; DESIGN APPROACHES; DUAL STAGES; FLEXIBLE SPACECRAFT; HYBRID APPROACHES; HYBRID CONTROL SCHEMES; INDUCED VIBRATIONS; INPUT VOLTAGES; LYAPUNOV ANALYSIS; NUMERICAL RESULTS; PARAMETER VARIATIONS; PIEZO-CERAMICS; REACTION WHEELS; REAL APPLICATIONS; RIGID BODIES; SENSOR AND ACTUATORS; SENSORS AND ACTUATORS; SLIDING MODE TECHNIQUES; SLIDING MODES; SLIDING-MODE CONTROLS; STRAIN RATE FEEDBACKS; UPPER BOUNDS; VELOCITY TRACKING; VIBRATION; VIBRATION REDUCTIONS; VIBRATION SUPPRESSIONS; VIBRATION-DAMPING; VIRTUAL TORQUES;

SPACECRAFT;

EID: 62549140134     PISSN: 08931321     EISSN: None     Source Type: Journal    
DOI: 10.1061/(ASCE)0893-1321(2009)22:2(139)     Document Type: Article

References (30)

1. Bailey, T., and Hubbard, J. E. (1985). " Distributed piezoelectric-polymer active vibration control of a cantilever beam.." J. Guid. Control, 8 (5), 605-611.
2. Cheon, Y. J. (2002). " Sliding mode control of spacecraft with actuator dynamics.." Trans. Contr. Autom. Syst. Eng., 4 (2), 169-175.
3. Crassidis, J. L., and Landis Markley, F. (1996). " Sliding mode control using modified Rodrigues parameters.." J. Guid. Control Dyn., 19 (6), 1381-1383.
4. Di Gennaro, S. (2003). " Output stabilization of flexible spacecraft with active vibration suppression.." IEEE Trans. Aerosp. Electron. Syst., 39 (3), 747-759.
5. Drakunov, S. V., and Utkin, V. I. (1992). " Sliding mode control in dynamic systems.." Int. J. Control, 55, 1029-1037.
6. Fung, R. F., and Yang, R. T. (1998). " Application of VSC in position control of a nonlinear lector hydraulic velocity servo system.." Comput. Struct., 66 (4), 365-372.
7. Hu, Q. L., and Ma, G. F. (2005a). " Variable structure control and active vibration suppression of flexible spacecraft during attitude maneuver.." Aerosp. Sci. Technol., 9, 307-317.
8. Hu, Q. L., and Ma, G. F. (2005b). " Vibration suppression of flexible spacecraft during attitude maneuvers.." J. Guid. Control Dyn., 28 (2), 377-380.
9. Hu, Q. L., and Ma, G. F. (2006a). " Control of three-axis stabilized flexible spacecrafts using variable structure strategies subject to input nonlinearities.." J. Vib. Control, 12 (6), 659-681.
10. Hu, Q. L., and Ma, G. F. (2006b). " Optimal sliding mode maneuvering control and active vibration reduction of flexible spacecraft.." Proc. Inst. Mech. Eng., Part G-J. Aerosp. Eng., 220 (4), 317-335.
11. Hu, Q. L., and Ma, G. F. (2006c). " Spacecraft vibration suppression using variable structure output feedback control and smart materials.." ASME J. Vibr. Acoust., 128 (2), 221-230.
12. Hung, J. Y., Gao, W., and Hung, J. C. (1993). " Variable structure control: A survey.." IEEE Trans. Ind. Electron., IE-40 (1), 2-22.
13. Hwang, C. L. (1996). " Sliding mode control using time-varying switching gain and boundary layer for electrohydraulic position and differential pressure control.." IEE Proc.: Control Theory Appl., 143 (4), 325-333.
14. Iyer, A., and Singh, S. N. (1991). " Variable structure slewing control and vibration damping of flexible spacecraft.." Acta Astron., 25 (1), 1-9.
15. Kaplan, M. H. (1976). Modern spacecraft dynamics and control, Wiley, New York.
16. Krstic, M., Kanellakopoulos, I., and Kokotovic, P. (1995). Nonlinear and adaptive control design, Wiley, New York.
17. Lam, T. (2006). " New approach to mission design based on the fundamental equations of motion.." J. Aerosp. Eng., 19 (2), 59-67.
18. Lo, S. C., and Chen, Y. P. (1995). " Smooth sliding mode control for spacecraft attitude tracking maneuvers.." J. Guid. Control Dyn., 18 (6), 1345-1349.
19. Newman, S. M. (1992). " Active damping control of a flexible space structure using piezoelectric sensors and actuators.." Master's thesis, U.S. Naval Postgraduate School.
20. Oz, H., and Mostafa, O. (1988). " Variable structure control systems (VSCS) maneuvering of flexible spacecraft.." J. Astronaut. Sci., 36 (3), 311-344.
21. Park, G. S., and Hwang, D. H. (2002). " Robust controller design for a class of nonlinear robot manipulators with actuator dynamics.." Int. J. Syst. Sci., 33 (7), 557-565.
22. Schutte, A. D., and Dooley, B. A. (2005). " Constrained motion of tethered satellites.." J. Aerosp. Eng., 18 (4), 242-250.
23. Singh, S. N. (1987). " Robust nonlinear attitude control of flexible spacecraft.." IEEE Trans. Aerosp. Electron. Syst., 23 (3), 380-387.
24. Song, G., and Kotejoshyer, B. (2002). " Vibration reduction of flexible structures during slew operations.." Int. J. Acoust. Vib., 7 (2), 105-109.
25. Su, C. Y., and Stepanenko, Y. (1997). " Backstepping based hybrid adaptive control of manipulators incorporating actuator dynamics.." Int. J. Adapt. Control Signal Process., 11, 141-153.
26. Tao, G. (2003). Adaptive control design and analysis, Wiley, N.J.
27. Tzou, H. S. (1993). Piezpelectric shells-distributed sensing and control of continua, Kluwer Academic, London.
28. Udwadia, F. E. (2003). " A new perspective on the tracking control of nonlinear structural and mechanical systems.." Proc. R. Soc. London, Ser. A, 459, 1783-1800.
29. Won, C. C., Sulla, J. L., Sparks, D. W., and Belvin, W. K. (1994). " Application of piezoelectric devices to vibration suppression.." J. Guid. Control Dyn., 17 (6), 1333-1338.
30. Zeng, Y., Araujo, A. D., and Singh, S. N. (1999). " Output feedback variable structure adaptive control of a flexible spacecraft.." Acta Astron., 44 (1), 11-22.