Robust nonlinear sequential loop closure control design for an air-breathing hypersonic vehicle model

Proceedings of the American Control Conference

Volumn , Issue , 2008, Pages 3458-3463

  Fiorentini, Lisa ^a,c   Serrani, Andrea ^a   Bolender, Michael A ^b   Doman, David B ^b  

^a OHIO STATE UNIVERSITY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c Ohio State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK INDICATORS; CHLORINE COMPOUNDS; DYNAMICS; FEEDBACK; FLIGHT DYNAMICS; HYPERSONIC AERODYNAMICS; STATE FEEDBACK; VEHICLES;

AIR-BREATHING; ANGLE-OF-ATTACK; CONTROL DESIGNS; CONTROL-ORIENTED MODELING; DYNAMIC STATES; FIRST PRINCIPLES; HIGH-FIDELITY; HYPERSONIC VEHICLES; NON-MINIMUM PHASE; PARAMETER UNCERTAINTIES; REFERENCE TRAJECTORIES; SEQUENTIAL LOOP; SIMPLIFIED MODELS; SIMULATION RESULTS; STRONG COUPLINGS; TRACKING PERFORMANCES; VEHICLE DYNAMICS;

AIRCRAFT INSTRUMENTS;

EID: 52449124796     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/ACC.2008.4587028     Document Type: Conference Paper

References (11)

1. C. Tournes, D. B. Landrum, Y. Shtessel, and C. W. Hawk, "Ramjet-powered reusable launch vehicle control by sliding modes," AIAA Journal of Guidance, Control, and Dynamics, vol. 21, no. 3, pp. 409-15, 1998.
2. D. B. Doman and A. D. Ngo, "Dynamic inversion-based adaptive/reconfigurable control of the X-33 on ascent," AIAA Journal of Guidance, Control, and Dynamics, vol. 25, no. 2, pp. 275-84, 2002.
3. Q. Wang and R. Stengel, "Robust nonlinear control of a hypersonic aircraft," AIAA Journal of Guidance, Control, and Dynamics, vol. 23, no. 4, pp. 577-85, 2000.
4. H. Xu, M. Mirmirani, and P. Ioannou, "Adaptive sliding mode control design for a hypersonic flight vehicle," AIAA Journal of Guidance, Control, and Dynamics, vol. 27, no. 5, pp. 829-38, 2004.
5. J. T. Parker, A. Serrani, S. Yurkovich, M. A. Bolender, and D. B. Doman, "Control-oriented modeling of an air-breathing hypersonic vehicle," Journal of Guidance, Control, and Dynamics, vol. 30, no. 3, pp. 856-869, 2007.
6. M. A. Bolender and D. B. Doman, "A nonlinear longitudinal dynamical model of an air-breathing hypersonic vehicle," Journal of Spacecraft and Rockets, vol. 44, no. 2, pp. 374-387, 2007.
7. L. Fiorentini, A. Serrani, M. Bolender, and D. Doman, "Nonlinear robust/adaptive controller design for an air-breathing hypersonic vehicle model," in AIAA Guidance, Navigation and Control Conference and Exhibit, Hilton Head, SC, 2007, AIAA Paper 2007-6329.
8. T. Williams, M. A. Bolender, D. B. Doman, and O. Morataya, "An aerothermal flexible mode analysis of a hypersonic vehicle," in AIAA Atmospheric Flight Mechanics Conference and Exhibit, Keystone, CO, Aug. 2006, AIAA Paper 2006-6647.
9. J. Schierman, D. Ward, J. Hull, N. Gandhi, M. Oppenheimer, and D. Doman, "Integrated adaptive guidance and control for re-entry vehicles with flight-test results," AIAA Journal of Guidance, Control, and Dynamics, vol. 27, no. 6, pp. 975-88, 2004.
10. H. K. Khalil, "Adaptive output feedback control of nonlinear systems represented by input-output models," IEEE Transactions on Automatic Control, vol. 41, no. 2, pp. 177-88, 1996.
11. H. Khalil, Nonlinear Systems, 3rd ed. Upper Saddle River, NJ: Prentice Hall, 2002.