Adaptive control of nonlinear attitude motions realizing linear closed loop dynamics

Journal of Guidance, Control, and Dynamics

Volumn 24, Issue 1, 2001, Pages 95-100

  Schaub, Hanspeter ^a   Akella, Maruthi R ^b   Junkins, John L ^c  

^a SANDIA NATIONAL LABORATORIES   (United States)

^b UNIVERSITY OF TEXAS AT AUSTIN   (United States)

^c TEXAS A AND M UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; ALGORITHMS; ASYMPTOTIC STABILITY; BANDWIDTH; CLOSED LOOP CONTROL SYSTEMS; ERROR ANALYSIS;

EULER PARAMETERS; MODIFIED RODRIGUES PARAMETERS (MRP);

MOTION CONTROL;

EID: 0034823590     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4680     Document Type: Article

References (30)

1. Wie, B., and Barba, P., "Quaternion Feedback for Spacecraft Large Angle Maneuvers," Journal of Guidance, Control, and Dynamics, Vol. 8, No. 3, 1985, pp. 360-365.
2. Wie, B., Weiss, H., and Arapostathis, A., "Quaternion Feedback Regulator Spacecraft Eigenaxis Rotations," Journal of Guidance, Control, and Dynamics, Vol. 12, No. 3, 1989, pp. 375-380.
3. Dwyer, T. A. W., "Exact Nonlinear Control of Spacecraft Slewing Maneuvers with Internal Momentum Transfer," Journal of Guidance, Control, and Dynamics, Vol. 9, No. 2, 1986, pp. 240-247.
4. Dwyer, T. A. W., "Exact Nonlinear Control of Large Angle Rotational Maneuvers," IEEE Transactions on Automatic Control, Vol. AC-29, No. 9, 1984, pp. 769-774.
5. Slotine, J. E., and Li, W., Applied Nonlinear Control, Prentice-Hall, Englewood Cliffs, NJ, 1991, pp. 12-85.
6. Schaub, H., and Junkins, J. L., "Stereographic Orientation Parameters for Attitude Dynamics: A Generalization of the Rodrigues Parameters," Journal of the Astronautical Sciences, Vol. 44, No. 1, 1996, pp. 1-19.
7. Shuster, M. D., "A Survey of Attitude Representations," Journal of the Astronautical Sciences, Vol. 41, No. 4, 1993, pp. 439-517.
8. Marandi, S. R., and Modi, V. J., "A Preferred Coordinate System and the Associated Orientation Representation in Attitude Dynamics," Acta Astronautica, Vol. 15, No. 11, 1987, pp. 833-843.
9. Tsiotras, P., "Stabilization and Optimality Results for the Attitude Control Problem," Journal of Guidance, Control, and Dynamics, Vol. 19, No. 4, 1996, pp. 772-779.
10. Robinett, R. D., Parker, G. G., Schaub, H., and Junkins, J. L., "Lyapunov Optimal Saturated Control for Nonlinear Systems," 35th Aerospace Sciences and Meeting, Reno, NV, 1997, Paper 97-0112.
11. Junkins, J. L., Akella, M. R., and Robinett, R. D., "Nonlinear Adaptive Control of Spacecraft Maneuvers," Journal of Guidance, Control, and Dynamics, Vol. 20, No. 6, 1997, pp. 1104-1110.
12. Akella, M., Junkins, J., and Robinett, R., "Structured Model Reference Adaptive Control with Actuator Saturation Limits," AIAA Guidance and Control Conference, Boston, 1998, Paper AAS 98-4472.
13. Schaub, H., Robinett, R. D., and Junkins, J. L., "Globally Stable Feedback Laws for Near-Minimum-Fuel and Near-Minimum-Time Pointing Maneuvers for a Landmark-Tracking Spacecraft," Journal of the Aeronautical Sciences, Vol. 44, No. 4, 1996, pp. 443-466.
14. Wen, J. T.-Y., and Kruetz-Delgado, K., "The Attitude Control Problem," IEEE Transactions on Automatic Control, Vol. AC-36, No. 10, 1991, pp. 1148-1162.
15. Joshi, S., Kelkar, A., and Wen, J. T.-Y., "Robust Attitude Stabilization of Spacecraft Using Nonlinear Quaternion Feedback," IEEE Transactions on Automatic Control, Vol. AC-40, No. 10, 1995, pp. 1800-1803.
16. Meyer, G., "On the Use of Euler's Theorem on Rotations for the Synthesis of Attitude Control Systems," NASA TN D-3643, 1966.
17. Meyer, G., "Design and Global Analysis of Spacecraft Attitude Control Systems," NASA TR R-361, 1971.
18. Reyhanoglu, M., van der Schaft, A., McClamroch, N., and Kalmanovsky, I., "Dynamics and Control of a Class of Underactuated Mechanical Systems," IEEE Transactions on Automatic Control, Vol. AC-44, No. 9, 1999, pp. 1663-1671.
19. Paielli, R. A., and Bach, R. E., "Attitude Control with Realization of Linear Error Dynamics," Journal of Guidance, Control, and Dynamics, Vol. 16, No. 1, 1993, pp. 182-189.
20. Narendra, K. S., and Annaswamy, A., Stable Adaptive Systems, Prentice-Hall, Englewood Cliffs, NJ, 1989, pp. 18-161.
21. Sastry, S., and Bodson, M., Adaptive Control: Stability, Convergence and Robustness, Prentice-Hall, Upper Saddle River, NJ, 1989, pp. 14-156.
22. Creamer, G., Delahunt, P., Gates, S., and Levenson, M., "Attitude Determination and Control of Clementine During Lunar Mapping," Journal of Guidance, Control, and Dynamics, Vol. 19, No. 3, 1996, pp. 505-511.
23. Cristi, R., and Burl, J., "Adaptive Eigenaxis Rotations," Proceedings of the European Control Conference, Groningen, The Netherlands, 1993, pp. 243-247.
24. Ahmed, J., Coppola, V., and Bernstein, D., "Adaptive Asymptotic Tracking of Spacecraft Attitude Motion with Inertia Matrix Identification," Journal of Guidance, Control, and Dynamics. Vol. 21, No. 5, 1998, pp. 684-691.
25. Schaub, H., "Novel Coordinates for Nonlinear Multibody Motion with Applications to Spacecraft Dynamics and Control," Ph.D Dissertation, Dept. of Aerospace Engineering, Texas A&M Univ., College Station, TX, May 1998.
26. Milenkovic, V., "Coordinates Suitable for Angular Motion Synthesis in Robots," Proceedings of Robots VI Conference, 1982, Paper MS82-217.
27. Tsiotras, P., "A Passivity Approach to Attitude Stabilization Using Nonredundant Kinematic Parameterizations," Proceedings of the 34th IEEE Conference on Decision and Control, 1995, pp. 515-520.
28. Junkins, J. L., and Kim, Y. Introduction to Dynamics and Control of Flexible Structures, AIAA Education Series, Washington DC, 1993, p. 81.
29. Gantmacher, The Theory of Matrices, Vol. 1, Chelsea, New York, 1977, pp. 353, 354.
30. Ioannou, P. A., and Sun, J., Stable and Robust Adaptive Control, Prentice-Hall, Englewood Cliffs, NJ, 1995, pp. 85-134.