Reconfigurable control design for the full X-33 flight envelope

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2001, Pages

  Christopher Cotting, M ^a   Burken, John J ^a  

^a NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894488504     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Wagner, Elaine A., John J. Burken, Curtis E. Hanson, and Jerry M. Wohletz Deterministic Reconfigurable Control Design For the X-33 Vehicle AIAA-98-4413, Aug. 1999.
2. Virnig, John C. and David S. Bodden Multivariable Control Allocation and Control Law Conditioning When Control Effectors Limit AIAA-94-3609, Aug. 1994.
3. Fletcher, R. and M. J. D. Powell A Rapidly Convergent Descent Method for Minimization The Complete Journal, vol. 6, no. 2, July 1963, pp. 163-168.
4. Fletcher, R., Practical Methods of Optimization: Volume 1, Unconstrained Optimization, John Wiley & Sons, Chichester, 1980.
5. Nonlinear Control Design Blockset, The Math Works Inc., Natick, Mass., 1997.
6. Hall, Charles E., Michael W. Gallaher, Neal E. Hendrix X-33 Attitude Control System Design for Ascent, Transition, and Entry Flight Regimes AIAA-98-4411, Aug. 1998.