Reconfigurable control design for the X-40A with in-flight simulation results

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference

Volumn 2, Issue , 2004, Pages 1371-1379

  Oppenheimer, Michael W ^a,b   Donian, David B ^a,b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b Bldg 146 ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; ALGORITHMS; ARCHITECTURAL DESIGN; COMPUTER SIMULATION; CONTROL THEORY; FLIGHT DYNAMICS; MANEUVERABILITY; MATRIX ALGEBRA; OPTIMIZATION; SIMULATORS; SPACE RESEARCH; VECTORS;

CONTROL LAWS; VEHICLE DYNAMICS; VELOCITY VECTORS; YAWNING RATES;

REMOTELY OPERATED VEHICLES;

EID: 19644394718     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-5017     Document Type: Conference Paper

References (7)

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2. A. B. Page and M. L. Steinberg, "A Closed-loop Comparison of Control Allocation Methods," in Proceedings of the 2000 Guidance, Navigation and Control Conference, AIAA 2000-1538, August 2000.
3. M. Bodson, "Evaluation of optimization methods for control allocation," Journal of Guidance, Control and Dynamics, vol. 25, no. 4, pp. 703-711, 2002.
4. J. D. Schierman, J. R. Hull, and D. G. Ward, "Adaptive Guidance With Trajectory Reshaping For Reusable Launch Vehicles," in Proceedings of the 2002 Guidance, Navigation and Control Conference, AIAA 2002-4458. August 2002.
5. B. Etkin, Dynamics of Atmospheric Flight. John Wiley & Sons, Inc., 1972.
6. D. B. Doman and M. W. Oppenheimer, "Improving Control Allocation Accuracy for Nonlinear Aircraft Dynamics," in Proceedings of the "2002 Guidance, Navigation and Control Conference, AIAA 2002-4667, August 2002.
7. J. D. Schierman, N. Gandhi, J. R. Hull, and D. G. Ward, "Flight Test Results Of An Adaptive Guidance System For Reusable Launch Vehicles," in Proceedings of the 2004 Guidance, Navigation and Control Conference, AIAA 2004-4771, August 2004.