Maneuvering flight control

Journal of Guidance, Control, and Dynamics

Volumn 21, Issue 3, 1998, Pages 368-374

  Pachter, M ^a,c   Chandler, P R ^b,c   Smith, L ^b  

^a AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; ADAPTIVE CONTROL SYSTEMS; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; FEEDBACK; FIGHTER AIRCRAFT; FLIGHT DYNAMICS; IDENTIFICATION (CONTROL SYSTEMS); LINEAR PROGRAMMING; LINEARIZATION; MATHEMATICAL MODELS; OPTIMAL CONTROL SYSTEMS;

ACTUATOR RATE SATURATION; VELOCITY VECTOR ROLL;

NONLINEAR CONTROL SYSTEMS;

EID: 0032074836     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4264     Document Type: Article

References (10)

1. Pachter, M., Chandler, P. R., and Mears, M., "Modeling and Control of Velocity Vector Rolls," Proceedings of the AIAA Guidance, Navigation, and Control Conference, AIAA, Washington, DC, 1995, pp. 20-37 (AIAA Paper 95-3177, Aug. 1995).
2. Pachter, M., and Chandler, P. R., "Velocity Vector Roll Control," AIAA Paper 96-3867, Aug. 1996.
3. Boyum, K. E., Pachter, M., and Houpis, C. H., "High Angle of Attack Velocity Vector Rolls," Control Engineering Practice, Vol. 3, No. 8, 1995, pp. 1087-1093.
4. Pachter, M., Chandler, P. R., and Mears, M., "Reconfigurable Tracking Control with Saturation," Journul of Guidance, Control, and Dynamics, Vol. 18, No. 5, 1995, pp. 1016-1022.
5. Smith, L., Chandler, P., and Pachter, M., "Regularization Techniques for Real-Time Identification of Aircraft Parameters," Proceedings of the AIAA Guidance, Navigation, and Control Conference (New Orleans, LA), AIAA, Reston, VA, 1997, pp. 1466-1480 (AIAA Paper 97-3740).
6. Stevens, B. L., and Lewis, F. L., Aircraft Control and Simulation, Wiley, New York, 1992, p. 141.
7. Simulation/Rapid-Prototyping Facility," Century Computing, Inc., Sun/ Unix version, Dayton, OH, Oct. 1992.
8. Blakelock, J. H., Automatic Control of Aircraft and Missiles, 2nd ed., Wiley, New York, 1991.
9. Pachter, M., D'Azzo, J. J., and Veth, M., "Proportional and Integral Control of Nonlinear Systems," International Journal of Control, Vol. 64, No. 4, 1996, pp. 679-692.
10. Hoak, D. E., and Fink, R. D., "USAF Stability and Control Digital DATCOM," U.S. Air Force Flight Dynamics Lab., AFFDL-TR-79-3032, Wright-Patterson AFB, OH, April 1979.