Methodologies for adaptive flight envelope estimation and protection

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2009, Pages

  Tang, Liang ^a   Roemer, Michael ^a   Ge, Jianhua ^a   Crassidis, Agamemnon ^b   Prasad, J V R ^c   Belcastro, Christine ^d  

^a IMPACT TECHNOLOGIES LLC   (United States)

^b ROCHESTER INSTITUTE OF TECHNOLOGY   (United States)

^c GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

^d NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; ADAPTIVE CONTROL SYSTEMS; AIRCRAFT CONTROL; AIRCRAFT DETECTION; DAMAGE DETECTION; DAMAGE TOLERANCE; DECISION SUPPORT SYSTEMS; FAULT DETECTION; INTERACTIVE COMPUTER SYSTEMS; NASA; REAL TIME SYSTEMS; RELIGIOUS BUILDINGS; TRAINING AIRCRAFT;

ENVELOPE ESTIMATION; FAULT DETECTION ALGORITHM; FLIGHT CONTROL ACTUATORS; GENERIC TRANSPORT MODELS; PERFORMANCE LIMITATIONS; REAL TIME DECISIONS; SIMULATION ENVIRONMENT; VEHICLE CONFIGURATION;

FLIGHT ENVELOPES;

EID: 78049290453     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-6260     Document Type: Conference Paper

References (22)

1. Shah, G., Aerodynamic Effects and Modeling of Damage to Transport Aircraft, AIAA Guidance, Navigation and Control Conference and Exhibit, 18-21 Aug 2008, Honolulu, Hawaii.
2. Bacon, B. J., and Gregory, I. M., General Equations of Motion for a Damaged Asymmetric Aircraft, AIAA Atmospheric Flight Mechanics Conference and Exhibit, 20-23 August 2007, Hilton Head, South Carolina.
3. Nguyen, N., Krishnakumar, K., Kaneshige, J., and Nespeca, P., Flight Dynamics and Hybrid Adaptive Control of Damaged Aircraft, Journal of Guidance, Control, and Dynamics, Vol. 31, No. 3, Pp 751-764, May-June 2008.
4. Murch, A. M., and Foster, J. V., Recent NASA Research on Aerodynamic Modeling of Post-Stall and Spin Dynamics of Large Transport Airplanes, 45th AIAA Aerospace Sciences Meeting and Exhibit, 8-11 Jan 2007, Reno, Nevada.
5. Goman, M. G., Khramtsovsky, A. V., and Kolesnikov, E. N., Evaluation of Aircraft Performance and Maneuverability by Computation of Attainable Equilibrium Sets, Journal of Guidance, Control, and Dynamics, Vol. 31, No. 2, Pp. 329-339, March-April 2008.
6. Lygeros, J., On reachability and minimum cost optimal control, Automatica, Volume 40, Issue 6, Pages 917-927, June 2004.
7. Mitchell, I. M., The flexible, extensible and efficient toolbox of level set methods, J. of Scientific Computing, vol. 35, no. 2-3, pp. 300-329, 2008.
8. Urnes, J. M., Reichenbach, Sr. E. Y., and Smith, T. A., Dynamic Flight Envelope Assessment and Prediction, AIAA Guidance Navigation and Control Conference, 18-21 August 2008, Honolulu, Hawaii.
9. Shin, J. and Belcastro, C., Robustness Analysis and Reliable Flight Regime Estimation of an Integrated Resilent Control System for A Transport Aircraft, AIAA Guidance Navigation and Control Conference, 18-21 August 2008, Honolulu, Hawaii.
10. Lombaerts, T. J. J., Huisman, H. O., Chu, Q. P., Mulder, J. A., and Joosten, D. A., Nonlinear Reconfiguring Flight Control Based on Online Physical Model Identification, Journal of Guidance, Control, and Dynamics, Vol. 32, No. 3, Pp 727-748, May-June 2009.
11. Yavrucuk, I., Prasad, J. V. R., and Unnikrishnan, S., Envelope Protection for Autonomous Unmanned Aerial Vehicles, Journal of Guidance, Control, and Dynamics, Vol. 32, No. 1, Pp 248-261, January-February 2009.
12. Tang, Y., Atkins, E. M., and Sanner, R. M., Emergency Flight Planning for a Generalized Transport Aircraft with Left Wing Damage, AIAA Guidance, Navigation and Control Conference and Exhibit, 20-23 August 2007, Hilton Head, South Carolina.
13. Byington, C.S., Watson, M., Edwards, D. and Stoelting, P., A model-based approach to prognostics and health management for flight control actuators, IEEE Aerospace Conference, Big Sky, Montana, 6-13 March 2004.
14. Balaban, E., Saxena, A., Bansal, P., Goebel, K.F., Stoelting, P., "A Diagnostic Approach for Electro-Mechanical Actuators in Aerospace Systems," IEEE Sensors Journal (accepted for publication)
15. Zhang, X., Polycarpou, M. M., and Parisini, T., Design and analysis of a fault isolation scheme for a class of uncertain nonlinear systems, IFAC Annual Reviews in Control, Volume 32, Issue 1, pp. 107-121, 2008.
16. Tang, L., Roemer, M., Bharadwaj, S., and Belcastro, C., An Integrated Aircraft Health Assessment and Fault Contingency Management System, AIAA Guidance, Navigation and Control Conference and Exhibit, Honolulu, Hawaii, 18 - 21 Aug 2008.
17. Unnikrishnan, S., Prasad, J.V.R. and Yavrucuk, I., Flight Evaluation of Reactionary Envelope Protection System for UAVs, Accepted for publication in the Journal of the American Helicopter Society, 2009.
18. Funahashi, K, On the Approximate Realization of a Continuous Mappings by Neural Nets, Neural Networks, vol. 2, issue 3, (1989) pp. 183-192.
19. Morelli, E. A., and Smith, M. S., Real-time dynamic modeling - data information requirements and flight test results, AIAA Atmospheric Flight Mechanics Conference and Exhibit, 18-21 August 2008, Honolulu, Hawaii.
20. Bailey, R. M., Hostetler, R. W., Barnes, K. N., Belcastro, C. M., and Belcastro, C. M., Experimental Validation: Subscale Aircraft Ground Facilities and Integrated Test Capability, AIAA Guidance, Navigation, and Control Conference, Washington, DC, 2005
21. Murch, A. M., A flight control system architecture for the NASA AirSTAR flight test infrastructure, AIAA Guidance, Navigation, and Control Conference and Exhibit, 18-21 August 2008, Honolulu, Hawaii.
22. Crassidis, A. L., Identification Update of Aerodynamic Models with Sensor Consistency Checks, AIAA Atmospheric Flight Mechanics Conference and Exhibit, 16-19 August 2004, Providence, Rhode Island.