Optimization and comparison of alternative flight control system design methods using a common set of handling-qualities criteria

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2001, Pages

  Tischler, Mark B ^a   Lee, James A ^b   Colbourne, Jason D ^a  

^a US Army AMRDEC Development   (United States)

^b University of Southern California   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 78651088235     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

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4. Tischler, M. B., et al, "A Multidisciplinary Flight Control Development Environment and Its Application to a Helicopter", IEEE Control Systems Magazine, Vol. 19, No. 4, August, 1999, pp. 22-33.
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11. Lane, S. H. and Stengel, R. F., "Flight Control Design Using Non-Linear Inverse Dynamics," Automatica, Vol 24, No. 4, 1988.
12. Franklin, J. A., "Attitude Control Augmentation and Tracking Display for XV15," NASA TM- 209599, Sept. 2000.
13. Schumacher, C., "Missile Autopilot Designs Using H-infinity Control and Dynamic Inversion," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 2, March-April, 1998.
14. Postlethwaite, I., Multivariable Feedback Control, Wiley, 1996, pp. 384-388.