Reconfigurable control design for the full X-33 flight envelope
Author:
Affiliation:
1. NASA, Dryden Flight Research Center, Edwards, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-4379
Reference6 articles.
1. 2Virnig,John C. and David S. Bodden,"Multivariable ControlAllocationand ControlLaw ConditioningWhen ControlEffectors Limit,"AIAA-94-3609,Aug.1994.
2. A Rapidly Convergent Descent Method for Minimization
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