Implementation of pilot commands in aircraft control: A new approach based on dynamic inversion

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2003, Pages

  Padhi, Radhakant ^a   Balakrishnan, S N ^a  

^a Architectural and Environmental Engineering   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPARISON STUDY; CONTROL SYNTHESIS; DESIGN PARAMETERS; DYNAMIC INVERSION; LATERAL ACCELERATION; LONGITUDINAL MODES; NUMERICAL RESULTS; OSCILLATORY RESPONSE;

AIRCRAFT CONTROL; NUMERICAL METHODS; TRANSPORT AIRCRAFT;

FLIGHT DYNAMICS;

EID: 84896693771     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (19)

1. Al-Hiddabi S. A. and McClamroch N. H., Aggressive Longitudinal Aircraft Trajectory Tracking Using Nonlinear Control, Journal of Guidance, Control and Dynamics, Vol.25, No.1, 2002, pp.26-32.
2. Asseo S. J., Application of Optimal Control of Perfect Model Following, Journal of Aircraft, Vol.7, July-Aug.,1970, pp.308-313.
3. Bryson A. E. and Ho Y. C., Applied Optimal Control, Taylor and Francis, 1975.
4. Enns D., Bugajski D., Hendrick R. and Stein G., Dynamic Inversion: An Evolving Methodology for Flight Control Design, International Journal of Control, Vol.59, No.1,1994, pp.71-91.
5. Ferrari S. and Stengel R., An Adaptive Critic Global Controller, Proceedings of the American Control Conference, 2002, pp. 2665-260.
6. Gupta S. K., Numerical Methods for Engineers, Wiley Eastern Limited, 1995.
7. Huang C. Y. and Stengel R. F., Restructurable Control Using Proportional-Integral Implicit Model Following, Journal of Guidance, Control and Dynamics, Vol.13, No.2, 1990, pp.303-309.
8. Hunt K. J., Neural Networks for Control Systems - A Survey, Automatica, Vol. 28, No. 6, 1992, pp. 1083-1112.
9. Jiang Z. P., Global Tracking Control of Underactuated Ships By Lyapunov's Direct Method, Automatica, Vol. 38, 2002, pp.301-309.
10. Kaneshige J., Bull J. and Totah J. J., Generic Neural Flight Control and Autopilot System, Proceedings of the AIAA Conference on Guidance, Navigation and Control, AIAA-2000-4281.
11. Khalil H. K., Nonlinear Systems, 3rd Edition, Prentice Hall, 2002.
12. Kim B. and Calise A. J., Nonlinear Flight Control Using Neural Networks, Journal of Guidance, Control and Dynamics, Vol.20, No.1, 1997, pp.26-33.
13. Lane S. H. and Stengel R. F., Flight Control Using Non-Linear Inverse Dynamics, Automatica, Vol.24, No.4, 1988, pp.471-483.
14. Menon P.K.A, Nonlinear Command Augmentation System for a High Performance Aircraft, Proceedings of the AIAA Conference on Guidance, Navigation and Control, 1993, AIAA-93-3777-CP.
15. Ngo A. D., Reigelsperger W. C. and Banda S. S., Multivariable Control Law Design for A Tailless Airplanes, Proceedings of the AIAA Conference on Guidance, Navigation and Control, 1996, AIAA-96- 3866.
16. Roskam J., Airplane Flight Dynamics and Automatic Controls (Part-I), Darcorporation, 1995.
17. Slotine J-J. E. and Li W., Applied Nonlinear Control, Prentice Hall, 1991.
18. Soloway D. and Haley P., Aircraft Reconfiguration Using Neural Generalized Predictive Control, Proceedings of The American Control Conference, 2001, pp. 2924-2929.
19. Stevens B. L. and Lewis F. L., Aircraft Control and Simulation: Wiley, 1992.