Stability Analysis of a Simplified Pitch-Controlled Flexible Aerodynamic Vehicle Via Lyapunov's Direct Method

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Report Number: AFFDL TR 65-145 p. 72-83
Author(s): Wang, P. K. C.
Corporate Author(s): IBM San Jose Research Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-11-01
Pages: 12
Contract: AF 33(657)-11545
DoD Project: 8225
DoD Task: 822501
Identifier: This paper is part of a conference proceedings. See AD0627048

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Provenance: AFRL/VACA

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