Sliding mode techniques applied to the control of a micro-air vehicle

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2003, Pages

  Hess, R A ^a   Ussery, T M ^a  

^a Davis   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AIRCRAFT CONTROL; CONTROLLERS; DEGREES OF FREEDOM (MECHANICS); DYNAMICS; FLIGHT SIMULATORS; SLIDING MODE CONTROL;

ASYMPTOTIC OBSERVER; DUCTED FAN; LOOP-SHAPING TECHNIQUE; SIX-DEGREE-OF-FREEDOM MODELING; SLIDING MODE CONTROLLER; SLIDING MODE TECHNIQUES; SLIDING MODES; VEHICLE DYNAMICS;

MICRO AIR VEHICLE (MAV);

EID: 85088723469     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-5408     Document Type: Conference Paper

References (11)

1. Lipera, L., Colbourne, J. D., Tischler, M. B., Mansur, M. H., Rotkowitz, M. C., and Patangui, P., "The Micro Craft iSTAR Micro Air Vehicle: Control System Design and Testing," American Helicopter Society 57th Annual Forum, Washington, DC, May 9-11, 2001.
2. Young, K. D., Utkin, V. I., and Ozguner, U., "A Control Engineer's to Sliding Mode Control," IEEE Transactions on Control Systems Technology, Vol. 7, No. 3, 1999, pp. 328-342.
3. Edwards, C., and Spurgeon, S. K., Sliding Mode Control, Taylor & Francis Ltd, Bristol, PA, 1998, Chap. 3.
4. Slotine, J.-J. E., and Li, W., Applied Nonlinear Control, Prentice Hall, Englewood Cliffs, NJ, 1991, Chap. 6.
5. Hess, R. A., and Wells, S. R., "Sliding Mode Control Applied to Reconfigurable Flight Control Design," Journal of Guidance, Control, and Dynamics, Vol. 26, No. 3, 2003, pp. 452-462.
6. Wells, R. A., and Hess, R. A., "MIMO Sliding Mode Control for a Tailless Fighter Aircraft," Journal of Guidance, Control, and Dynamics, Vol. 26, No. 3, 2003, pp. 463-473.
7. Vetter, T. K., Hess, R. A., and Wells, S. R. "Designing for Damage - Robust Flight Control Design Using Sliding Mode Techniques," Journal of Aerospace Engineering, Institution of Mechanical Engineers, UK, submitted.
8. Wells, S. R., "Application of Sliding Mode Techniques to the Design of Reconfigurable Flight Control Systems," Ph.D. Dissertation, Dept. of Mechanical and Aeronautical Engineering, University of California, Davis, June 2002.
9. Maciejowski, J. M., Multivariable Feedback Design, Addison-Wesley, Wokingham, UK, 1989, Chap. 1.
10. McRuer, D., Ashkenas, I., and Graham, D., Aircraft Dynamics and Automatic Control, Princeton University Press, Princeton, NJ, 1973, p. 223.
11. Hess, R. A., "Rotorcraft Handling Qualities in Turbulence," Journal of Guidance, Control, and Dynamics, Vol. 18, No. 1, pp. 39-45, 1995.