Controlled dynamics of flexible orbiting tethered systems: Analysis and experiments

JVC/Journal of Vibration and Control

Volumn 3, Issue 4, 1997, Pages 459-497

  Modi, Vinod J ^a   Pradhan, Satyabrata ^a   Misra, Arun K ^b  

^a UNIVERSITY OF BRITISH COLUMBIA   (Canada)

^b MCGILL UNIVERSITY   (Canada)

Author keywords

Feedback linearization technique; Hybrid control; Tethered systems

Indexed keywords

DYNAMICS; FEEDBACK CONTROL; FLEXIBLE STRUCTURES; LAGRANGE MULTIPLIERS; LINEARIZATION;

FEEDBACK LINEARIZATION TECHNIQUE; HYBRIDE CONTROL; TETHERED SYSTEMS;

TETHERLINES;

EID: 0031273326     PISSN: 10775463     EISSN: None     Source Type: Journal    
DOI: 10.1177/107754639700300406     Document Type: Article

References (35)

1. Astrom, K. J. and Wittenmark, B., 1989, Adaptive Control, Addison-Wesley, Reading, MA.
2. Bainum, P. M. and Kumar, V. K., 1980, "Optimal-control of the shuttle-tethered system," Acta Astronautica 7(2), 1333-1348.
3. Baker, P. W., Dunkin, J. A., Galaboff, Z. J., Johnston, K. D., Kissel, R. R., Rheinfurth, M. H., and Siebel, M.P.L., 1976, "Tethered subsatellite study," NASA TM X-73314.
4. Balas, G. J., Garrard, W. L., and Reiner, J., 1992, "Robust dynamic inversion control laws for aircraft control," in Proceedings of the 1992 AIAA Guidance, Navigation, and Control Conference, Hilton Head Island, SC, August, pp. 192-205.
5. Banerjee, A. K. and Kane, T. R., 1984, "Tethered satellite retrieval with thruster augmented control," J. Guidance Control Dyn. 7(1), 45-50.
6. Bortolami, S. B., Lorenzini, E. C., Rupp, C. C., and Angrilli, F, 1993, "Control law for the deployment of SEDS-II," in Advances in Astronautical Sciences, A. K. Misra, V. J. Modi, R. Holdaway, and P. M. Bainum, eds., AAS Publication, San Diego, CA, pp. 733-748.
7. Chiang, R. Y. and Safonov, M. G., 1992, Robust Control Toolbox User's Guide, Math Works Inc., Natick, MA.
8. deSilva, C. W., 1989, Control Sensors and Actuators, Prentice Hall, Englewood Cliffs, NJ.
9. Doyle, J. C. and Stein, G., 1981, "Multivariable feedback design: Concepts for a classical/modern synthesis," IEEE Trans. Auto. Control 26(1), 4-16.
10. Gullahorn, G. E., Hohlfeld, R. G., and Bonifazi, C., 1993, "Observations of tethered satellite system (TSS-1) dynamics," in Advances in Astronautical Sciences, A. K. Misra, V. J. Modi, R. Holdaway, and P. M. Bainum, eds., AAS Publication, San Diego, CA, pp. 701-710.
11. Isidori, A., 1989, Nonlinear Control Systems: An Introduction, 2nd ed., Lecture Notes in Control and Information Sciences 72, Springer-Verlag, Berlin, pp. 145-281.
12. Karray, F, Modi, V. J., and Chan, J. K., 1991, "Inverse control of flexible orbiting manipulators," in Proceedings of the American Control Conference, Boston, MA, pp. 1909-1912.
13. Keshmiri, M. and Misra, A. K., 1993, "A general formulation for N-body tethered satellite system dynamics," in Advances in Astronautical Sciences, A. K. Misra, V. J. Modi, R. Holdaway, and P. M. Bainum, eds., AAS Publication, San Diego, CA, pp. 623-644.
14. Kohler, P., Maag, W., Wehrli, R., Weber, R., and Brauchli, H., 1978, "Dynamics of a system of two satellites connected by a deployable and extensible tether of finite mass," ESTEC Contract Report No. 2992/76/NL/Ak (sc), 1 and 2, Noordwijk, the Netherlands.
15. Lang, D. L. and Nolting, R. K., 1967, "Operations with tethered space vehicles," NASA SP-138, Gemini Summary Conference, February, pp. 55-64.
16. Misra, A. K. and Modi, V. J., 1978, "The influence of satellite flexibility on orbital motion," Celestial Mech. 17, 145-165.
17. Misra, A. K. and Modi, V. J., 1982, "Dynamics and control of tether connected two-body system - a brief review," Paper No. 82-315, 33rd Congress of the International Astronautical Federation, Paris, September. (Also in Space 2000, Selection of Papers From the 33rd IAF Congress, L. G. Napolitano, ed., AIAA Publishers, pp. 473-514.)
18. Misra, A. K. and Modi, V. J., 1982, "Dynamics and control of tether connected two-body system - a brief review," Paper No. 82-315, 33rd Congress of the International Astronautical Federation, Paris, September. (Also in Space 2000, Selection of Papers From the 33rd IAF Congress, L. G. Napolitano, ed., AIAA Publishers, pp. 473-514.)
19. Misra, A. K. and Modi, V. J., 1986, "A survey on the dynamics and control of tethered satellite systems," Paper No. AAS-86-246, NASA/AIAA/PSN International Conference on Tethers, Arlington, VA, September. (Also in Advances in the Astronautical Sciences, P. M. Bainum, I. Bekey, L. Guerriero, and P. A. Penzo, eds., AAS Publication, San Diego, CA, pp. 667-719.)
20. Misra, A. K. and Modi, V. J., 1986, "A survey on the dynamics and control of tethered satellite systems," Paper No. AAS-86-246, NASA/AIAA/PSN International Conference on Tethers, Arlington, VA, September. (Also in Advances in the Astronautical Sciences, P. M. Bainum, I. Bekey, L. Guerriero, and P. A. Penzo, eds., AAS Publication, San Diego, CA, pp. 667-719.)
21. Modi, V. J., Lakshmanan, P. K., and Misra, A. K., 1990, "Offset control of tethered satellite systems: Analysis and experimental verification," Acta Astronautica 21(5), 283-294.
22. Modi, V. J., Lakshmanan, P. K., and Misra, A. K., 1991, "On the control of tethered satellite systems," Paper No. AIAA-91-1002, Proceedings of the AIAA/ASME/ASCE/AHS/ASC 32nd Structures, Structural Dynamics, and Materials Conference, Baltimore, MD, April.
23. Pasca, M. and Lorenzini, E., 1991, "Collection of martian atmospheric dust with a low altitude tethered probe," Paper No. AAS 91-178, AAS/AIAA Spaceflight Mechanics Meeting, Houston, TX, February 11-13.
24. Pasca, M., Pignataro, M., and Luongo, A., 1991, "Three-dimensional vibrations of tethered satellite systems," J. Guidance Control Dyn. 14(2), 312-320.
25. Pradhan, S., 1994, "Planar dynamics and control of tethered satellite systems," Ph.D. thesis, Department of Mechanical Engineering, University of British Columbia, Vancouver, British Columbia, Canada, pp. 204-225.
26. Pradhan, S., Modi, V. J., and Misra, A. K., 1994, "On the inverse control of the tethered satellite systems," in Proceedings of the 19th International Symposium on Space Technology and Science, Yokohama, Japan, May, pp. 281-288.
27. Rupp, C. C., 1975, "A tether tension control law for tethered subsatellites deployed along local vertical," NASA TM X-64963.
28. Sasaki, S., Oyama, K. I., Kawashima, N., Watanabe, Y, Obayashi, T., Raitt, W. J., White, A. B., Banks, P. M., Williamson, P. R., Sharp, W. F., Yokota, T., and Hirao, K., 1987, "Results from a series of tethered rocket experiments," J. Spacecraft Rocket 24(5), 444-453.
29. Su, R., 1982, "On the linear equivalents of nonlinear systems," Systems Control Lett. 2(1), 48-52.
30. Sutton, G. W. and Diederich, F. W., 1967, "Synchronous rotation of a satellite at less than synchronous altitude," AIAA J. 5(4), 813-815.
31. Tyc, G., Han, R.P.S., Vigneron, F. R., Jablonski, A. M., Modi, V. J., and Misra, A. K., 1993, "Dynamics and stability of a spinning tethered spacecraft with flexible appendages," in Advances in Astronautical Sciences, A. K. Misra, V. J. Modi, R. Holdaway, and P. M. Bainum, eds., AAS Publication, San Diego, CA, pp. 877-896.
32. Vidyasagar, M. and Viswanatham, N., 1982, "Algebraic design techniques for reliable stabilization," IEEE Transactions on Automatic Control 27(10), 1085-1195.
33. Yasaka, T. and Hatsuda, T., 1988, "Geostationary tethered satellite system and its application to communication systems," IEEE Transactions on Aerospace and Electronics Systems 24(1), 68-75.
34. Yu, E. Y, 1964, "Long-term coupling effects between the librational and orbital motions of a satellite," AIAA J. 2(3), 553-555.
35. Yuan, J.S.C. and Stieber, M. E., 1986, "Robust beam-pointing and attitude control of a flexible spacecraft," J. Guidance Control Dyn. 9(2), 228-234.