Adaptive flight control for an autonomous unmanned helicopter

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2002, Pages

  Johnson, Eric N ^a   Kannan, Suresh K ^a  

^a Georgia Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; HELICOPTERS; UNMANNED AERIAL VEHICLES (UAV);

ADAPTIVE FLIGHT CONTROLS; AUTONOMOUS HELICOPTER FLIGHTS; AUTONOMOUS UNMANNED HELICOPTERS; FLIGHT CONTROL PROBLEMS; LINEARIZED SYSTEMS; PSEUDO-CONTROL HEDGING; TRACKING PERFORMANCE; TRANSLATIONAL DYNAMICS;

AIRCRAFT CONTROL;

EID: 85078724392     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-4439     Document Type: Conference Paper

References (15)

1. Frazzoli, E., Dahleh, M. A., and Feron, E., "Robust Hybrid Control for Autonomous Vehicles Motion Planning," Tech. Rep. LIDS-P-2468, Laboratory for Information and Decision Systems, Massachusetts Institute of Technology, Cambridge, MA, 1999.
2. Sanders, C., DeBitetto, P. D., Vuong, H. F., and Levenson, N., "Hierarchical Control of Small Autonomous Helicopters," IEEE Conference on Decision and Control, Tampa, Florida, 1998.
3. Rysdyk, R. T. and Calise, A. J., "Nonlinear Adaptive Flight Control Using Neural Networks," IEEE Controls Systems Magazine, Vol. 18, No. 6, dec 1998.
4. Shim, D. H., Koo, T. J., Hoffmann, F., and Sastry, S., "A comprehensive study of control design for an autonomous helicopter," IEEE Conference on Decision and Control, Dec. 1999.
5. Calise, A. J., Lee, H., and Kim, N., "High Bandwidth Adaptive Flight Control," AIAA Guidance, Navigation and Control Conference, Denver, CO, aug 2000.
6. Calise, A. J., Lee, S., and Sharma, M., "Development of a Reconfigurable Flight Control Law for Tailless Aircraft," AIAA Journal of Guidance, Control, and Dynamics, Vol. 24, No. 5, 2001, pp. 896-902.
7. Brinker, J. and Wise, K., "Flight testing of a reconfigurable flight control law on the X-36 tailless fighter aircraft," AIAA Journal of Guidance, Control, and Dynamics, Vol. 24, No. 5, 2001, pp. 903-909.
8. Johnson, E. N., Calise, A. J., and Corban, J. E., "Reusable Launch Vehicle Adaptive Guidance and Control Using Neural Networks," AIAA Guidance, Navigation and Control Conference, No. 4381, 2001.
9. Johnson, E. N., Limited Authority Adaptive Flight Control, Ph.D. thesis, Georgia Institute of Technology, School of Aerospace Engineering, Atlanta, GA 30332, dec 2000.
10. Stevens, B. L. and Lewis, F. L., Aircraft Control and Sim-ulaion, John Wiley & Sons, New York, 1992.
11. Johnson, E. N., Calise, A. J., El-Shirbiny, H. A., and Rysdyk, R. T., "Feedback Linearization with Neural Network Augmentation applied to X-33 Attitude Control," AIAA Guidance, Navigation and Control Conference, Denver, CO, aug 2000.
12. K. Hornik, M. Stinchombe, and H. White, "Multilayer Feedforward Networks are Universal Approximators," Neural Networks, Vol. 2, 1989, pp. 359-366.
13. Munzinger, C., Development of a Real-Time Flight Simulator for An Experimental Model Helicopter, Master's thesis, Georgia Institute of Technology, School of Aerospace Engineering, Atlanta, GA 30332, jul 1997.
14. Johnson, E. N. and DeBitetto, P. D., "Modelling and Simulation for Small Autonomous Helicopter Development," AIAA Modelling & Simulation Technologies Conference, Monterey, California, 1997.
15. Gavrilets, V., Mettler, B., and Feron, E., "Nonlinear Model for a Small-Sized Acrobatic Helicopter," AIAA Guidance, Navigation and Control Conference, No. 2001-4333, Montŕeal, Quebec, Canada, Aug. 2001.