On-line computation of a local attainable moment set for reusable launch vehicles

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2002, Pages

  Hodel, A S ^a   Shtessel, Yuri B ^b  

^a AUBURN UNIVERSITY   (United States)

^b UNIVERSITY OF ALABAMA IN HUNTSVILLE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

LAUNCH VEHICLES; LAUNCHING; REUSABILITY; REUSABLE ROCKETS;

COMPUTATIONAL COSTS; ONLINE COMPUTATIONS; REUSABLE LAUNCH VEHICLES;

LINEAR PROGRAMMING;

EID: 85085402586     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-4780     Document Type: Conference Paper

References (14)

1. Lu, P., Sun, H., and Tsai, B., Closed-Loop Endo-Atmospheric Ascent Guidance, Proceedings of the AIAA Guidance, Navigation and Control Conference and Exhibit, Monterey, CA, 2002, Paper number AIAA-2002-4558.
2. Shen, Z. and Lu, P., On-Board Generation of Three-Dimensional Constrained Entry Trajectories, Proceedings of the AIAA Guidance, Navigation and Control Conference and Exhibit, Monterey, CA, 2002, Paper number AIAA-2002-4455.
3. Shtessel, Y., Bungton, J., and Banda, S., Multiple Time Scale Flight Control Using Recon-gurable Sliding Modes, AIAA Journal on Guidance, Control, and Dynamics, Vol. 22, No. 6, 1999, pp. 873-883.
4. Shtessel, Y. and Krupp, D., Reusable Launch Vehicle Trajectory Control in Sliding Modes, Proceedings of the American Control Conference, Albuquerque, New Mexico, June 1997, pp. 2557-2561.
5. Shtessel, Y., Hall, C. E., and Jackson, M., Reusable Launch Vehicle Control in Multiple Time Scale Sliding Modes, Proceedings of AIAA Guidance, Navigation, and Control Conference, No. AIAA-2000-4155, AIAA, Denver, Co, August 14-17 2000.
6. Page, A. B. and Stenberg, M. L., A Closed-Loop Comparison of Control Allocation Methods, Proceedings of AIAA Guidance, Navigation, and Control Conference and Exhibit, American Institute of Aeronautics and Astronautics, Denver, Colorado, August 14-17 2000, Paper AIAA-2000-4538.
7. Hodel, A. S., Robust Inversion and Data Compression in Control Allocation, Proceedings of AIAA Guidance, Navigation, and Control Conference and Exhibit, American Institute of Aeronautics and Astronautics, Denver, Colorado, August 14-17 2000, Paper AIAA-2000-4154.
8. Fisher, J. E., Lawrence, D. A., and Zhu, J. J., Autocommander - A Supervisory Controller for Integrated Guidance and Control for the 2nd Generation Reusable Launch Vehicle, Proceedings of the AIAA Guidance, Navigation and Control Conference and Exhibit, Monterey, CA, 2002, Paper number AIAA-2002-4562.
9. Hodel, A. S. and Hall, C. E., Variable Structure PID Control to Prevent Integrator Windup, IEEE Trans. Indust. Elect., Vol. 48, No. 2, April 2001, pp. 442-451.
10. Bordignon, K. A. and Durham, W. C., Closed-Form Solutions to Constrained Control Allocation Problem, Journal of Guidance, Control, and Dynamics, Vol. 18, No. 5, September-October 1995, pp. 1000-1007.
11. Durham, W. C., Constrained Control Allocation, Journal of Guidance, Control, and Dynamics, Vol. 16, No. 4, August 1993, pp. 717-725.
12. Durham, W. C., Ecient, Near-Optimal Control Allocation, Journal of Guidance, Vol. 22, No. 2, 1999, pp. 369-372.
13. Boyd, S., El Ghaoui, L., Feron, E., and Balakrishnan, V., Linear Matrix Inequalities in System and Control Theory, SIAM, 1994.
14. nd ed., 1984. 15Karmarkar, N., A New Polynomial-Time Algorithm for Linear Programming, Combinatorica, Vol. 4, 1984, pp. 373-395.