Active vibration suppression in flexible spacecraft attitude tracking

Journal of Guidance, Control, and Dynamics

Volumn 21, Issue 3, 1998, Pages 400-408

  Di Gennaro, S ^a  

^a UNIVERSITY OF L'AQUILA   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; COMPUTER SIMULATION; DAMPING; FLIGHT DYNAMICS; MATHEMATICAL MODELS; PIEZOELECTRIC DEVICES; SPACECRAFT;

FLEXIBLE SPACECRAFT ATTITUDE TRACKING;

VIBRATION CONTROL;

EID: 0032071122     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4272     Document Type: Article

References (35)

1. Azain, M., Singh, S. N., Iyer, A., and Kakad, Y. P., "Detumbling and Reorientation Maneuvers and Stabilization of NASA SCOLE System," IEEE Transactions on Aerospace and Electronic Systems, Vol. 28, No. 1, 1992, pp. 80-91.
2. Azam, M., Singh, S. N., Iyer, A., and Kakad, Y. P., "Nonlinear Rotational Maneuver and Vibration Damping of NASA SCOLE System," Acta Astronautica, Vol. 32, No. 3, 1994, pp. 211-220.
3. Bach, R. E., and Paielli, R., "Linearization of Attitude-Control Error Dynamics," IEEE Transactions on Automatic Control, Vol. 38, No. 10, 1993, pp. 1521-1525.
4. Biswas, S. K., and Ahmed, N. U., "Stabilization of a Class of Hybrid Systems Arising in Flexible Spacecraft," Journal of Optimization Theory and Applications, Vol. 50, No. 1, 1986, pp. 83-108.
5. Dwyer, T. A. W., "Exact Nonlinear Control of Large Angle Rotational Maneuvers," IEEE Transactions on Automatic Control, Vol. 29, No. 9, 1984, pp. 769-774.
6. Dwyer, T. A. W., Sira-Ramirez, H., Monaco, S., and Stornelli, S., "Variable Structure Control of Globally Feedback-Decoupled Deformable Vehicle Maneuvers," Proceedings of the 26th IEEE Conference on Decision and Control (Los Angeles, CA), Inst. of Electrical and Electronics Engineers Service Center, Piscataway, NJ, 1987, pp. 1281-1287.
7. Hablani, H. B., "Multiaxis Tracking and Attitude Control of Flexible Spacecraft with Reaction Jets," Journal of Guidance, Control, and Dynamics, Vol. 17, No. 4, 1994, pp. 831-839.
8. Kakad, Y. P., "Slew Maneuvers of Spacecraft Control Laboratory Experiment (SCOLE)," NASA CR-190228, April 1992.
9. Monaco, S., and Stornelli, S., "A Nonlinear Feedback Control Law for Attitude Control," Algebraic and Geometric Methods in Nonlinear Control Theory, edited by M. Hazewinkel and M. Fliess, Reidel, Dordrecht, The Netherlands, 1985, pp. 573-595; also Univ. of Rome "La Sapienza," TR DIS-12.84, Rome, Italy, Dec. 1984.
10. Monaco, S., and Stornelli, S., "A Nonlinear Feedback Control Law for Attitude Control," Algebraic and Geometric Methods in Nonlinear Control Theory, edited by M. Hazewinkel and M. Fliess, Reidel, Dordrecht, The Netherlands, 1985, pp. 573-595; also Univ. of Rome "La Sapienza," TR DIS-12.84, Rome, Italy, Dec. 1984.
11. Monaco, S., and Stornelli, S., "A Nonlinear Attitude Control Law for a Satellite with Flexible Appendages," Proceedings of the 24th IEEE Conference on Decision and Control (Ft. Lauderdale, FL), Inst. of Electrical and Electronics Engineers Service Center, Piscataway, NJ, 1985, pp. 1654-1659.
12. Monaco, S., Normand-Cyrot, D., and Stornelli, S., "Sampled Nonlinear Control for Large Angle Maneuvers of Flexible Spacecraft," Proceedings of the 2nd International Symposium on Spacecraft Flight Dynamics (Darmstadt, Germany), European Space Agency, European Space Research and Technology Center, Noordwijk, The Netherlands, 1986, pp. 31-38 (ESA SP-255).
13. Monaco, S., Normand-Cyrot, D., and Stornelli, S., "On the Linearizing Feedback in Nonlinear Sampled Data Control Schemes," Proceedings of the 25th IEEE Conference on Decision and Control (Athens, Greece), Inst. of Electrical and Electronics Engineers Service Center, Piscataway, NJ, 1986, pp. 2056-2060.
14. Monaco, S., Normand-Cyrot, D., and Stornelli, S., "Multirate Three Axes Attitude Stabilization of Spacecraft," Proceedings of the 28th IEEE Conference on Decision and Control (Tampa, FL), Inst. of Electrical and Electronics Engineers Service Center, Piscataway, NJ, 1989, pp. 797-802.
15. Singh, S. N., "Robust Nonlinear Attitude Control of Flexible Spacecraft," IEEE Transactions on Aerospace and Electronic Systems, Vol. 23, No. 3, 1987, pp. 380-387.
16. Singh, S. N., "Rotational Maneuver of Nonlinear Uncertain Elastic Spacecraft," IEEE Transactions on Aerospace and Electronic Systems, Vol. 24, No. 2, 1988, pp. 114-123.
17. Wen, J. T., and Kreutz-Delgado, K., "The Attitude Control Problem," IEEE Transactions on Automatic Control, Vol. 36, No. 10, 1991, pp. 1148-1162.
18. Wie, B., and Barba, P. M., "Quaternion Feedback for Spacecraft Large Angle Maneuvers," Journal of Guidance, Control, and Dynamics, Vol. 8, No. 3, 1985, pp. 360-365.
19. Annaswamy, A. M., and Clancy, D. J., "Adaptive Control Strategies for Flexible Space Structures," IEEE Transactions on Aerospace and Electronic Systems, Vol. 32, No. 3, 1996, pp. 952-965.
20. Singh, S. N., "Nonlinear Adaptive Attitude Control of Spacecraft," IEEE Transactions on Aerospace and Electronic Systems, Vol. 23, No. 3, 1987, pp. 371-379.
21. Georgiou, G., Di Gennaro, S., Monaco, S., and Normand-Cyrot, D., "On the Nonlinear Adaptive Control of a Flexible Spacecraft," Proceedings of the 1st ESA Conference on Spacecraft Guidance, Navigation, and Control Systems (Noordwijk, The Netherlands), European Space Agency, European Space Research and Technology Center, Noordwijk, The Netherlands, 1991, pp. 509-514 (ESA SP-323).
22. Crawley, E. F., and de Luis, J., "Use of Piezoelectric Actuators as Elements of Intelligent Structures," AIAA Journal, Vol. 25, No. 10, 1987, pp. 1373-1385.
23. Yang, S. M., and Lee, Y. J., "Modal Analysis of Stepped Beams with Piezoelectric Materials," Journal of Sound and Vibration, Vol. 176, No. 3, 1994, pp. 289-300.
24. Baz, A., and Poh, S., "Performance of an Active Control System with Piezoelectric Actuators," Journal of Sound and Vibration, Vol. 126, No. 2, 1988, pp. 327-343.
25. Burke, S. E., and Hubbard, J. E., Jr., "Distributed Actuator Control Design for Flexible Beams," Automatica, Vol. 24, No. 5, 1988, pp. 619-627.
26. Li, Z., and Bainum, P. M., "Vibration Control of Flexible Spacecraft Integrating a Momentum Exchange Controller and a Distributed Piezoelectric Actuator," Journal of Sound and Vibration, Vol. 177, No. 4. 1994, pp. 539-553.
27. Bailey, T., and Hubbard, J. E., Jr., "Distributed Piezoelectric-Polymer Active Vibration Control of a Cantilever Beam," Journal of Guidance, Control, and Dynamics, Vol. 8, No. 5, 1985, pp. 605-611.
28. Hyland, D. C., Junkins, J. L., and Longman, R. W., "Active Control Technology for Large Space Structures," Journal of Guidance, Control, and Dynamics, Vol. 16, No. 5, 1993, pp. 801-821.
29. Ickes, B. P., "A New Method for Performing Digital Control System Attitude Computations Using Quaternions," AIAA Journal, Vol. 8, No. 1, 1970, pp. 13-17.
30. Yuan, J. S. C., "Closed-Loop Manipulator Control Using Quaternion Feedback," IEEE Journal of Robotics and Automation, Vol. 4, No. 4, 1988, pp. 434-440.
31. Meirovitch, L., Analytical Methods in Vibrations, Macmillan, New York, 1967.
32. Goldstein, H., Classical Mechanics, Addison-Wesley, Reading, MA, 1965.
33. Sastry, S. S., and Bodson, M., Adaptive Control: Stability, Convergence, and Robustness, Prentice-Hall, Englewood Cliffs, NJ, 1989.
34. Khalil, H. K., Nonlinear Systems, Macmillan, New York, 1992.
35. Curtain, R. F., and Pritchard, A. J., Functional Analysis in Modern Applied Mathematics, Academic, New York, 1977.