Enhancements to a neural adaptive flight control system for a modified F-15 aircraft

AIAA Guidance, Navigation and Control Conference and Exhibit

Volumn , Issue , 2008, Pages

  Kaneshige, John ^a,c   Burken, John ^b,d  

^a NASA AMES RESEARCH CENTER   (United States)

^b NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

^c Intelligent Systems Division   (United States)

^d Flight Controls Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE FLIGHT CONTROL SYSTEM; CONTROL SURFACE FAILURE; DAMAGE CONDITION; DAMPING CONTROLLERS; FLIGHT TEST; IMPROVING PERFORMANCE; INPUT SELECTION; INTELLIGENT FLIGHT CONTROL SYSTEMS; LEARNING RATES; NETWORK-BASED APPROACH; PILOT-INDUCED OSCILLATIONS; RESEARCH EFFORTS; SIMULATION RESULT;

AIRCRAFT CONTROL; COMPUTER SIMULATION; CONTROL SURFACES; FLIGHT CONTROL SYSTEMS; FLIGHT SIMULATORS; NASA; NAVIGATION; NEURAL NETWORKS; REMOTE CONTROL; RETROFITTING; ROBUSTNESS (CONTROL SYSTEMS); UNMANNED AERIAL VEHICLES (UAV);

ADAPTIVE CONTROL SYSTEMS;

EID: 78651087671     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

1. Hageman, J. J., Smith, M. S., and Stachowiak, S. J., "Integration of Online Parameter Identification and Neural Network for In-Flight Adaptive Control", NASA/TM-2003-212028, Oct. 2003.
2. Burken, J. J., Williams-Hayes, P., Kaneshige, J. T., and Stachowiak, S. J., "Reconfigurable Control with Neural Network Augmentation for a Modified F-15 Aircraft," NASA/TM-2006-213678, Apr. 2006.
3. Bosworth, J. T., and Williams-Hayes, P., "Flight Test Results from the NF-15B Intelligent Flight Control System (IFCS) Project with Adaptation to a Simulated Stabilator Failure," AIAA Infotech@Aerospace Conference, AIAA-2007-2818, May 2007.
4. Bomben, C. R., Smolka, J. W., Bosworth, J. T., Williams-Hayes, P., Burken, J. J., Larson, R. R., Buschbacher, M. J., and Maliska, H. A., "Development and Flight Testing of a Neural Network Based Flight Control System on the NF-15B Aircraft," 2006 Report to the Aerospace Profession Fiftieth Symposium Proceedings, 2006, pp. 214-240.
5. Calise, A. J., Lee, S., and Sharma, M., "Direct Adaptive Reconfigurable Control of a Tailless Fighter Aircraft," AIAA Guidance, Navigation, and Control Conference, AIAA-1998-4018, Aug. 1988.
6. Rysdyk, R. T., and Calise, A. J., "Fault Tolerant Flight Control Via Adaptive Neural Network Augmentation," AIAA Guidance, Navigation, and Control Conference, AIAA-1998-4483, Aug. 1988.
7. Flying Qualities of Piloted Vehicles, U.S. Department of Defense, MIL-STD-1797, March 31, 1987.