An analysis method based on simulation in the time and frequency domains is described for analyzing flutter of a missile fin actuator in the presence of nonlinearities. The method is illustrated by applying it to a hydraulic actuator with backlash and to a pneumatic actuator having nonlinear gas dynamics. All the work was done through computer simulation using the higher order language ACSL.
Nonlinear flutter analysis of a missile fin/actuator
Nichtlineare Schwankungsanalyse eines Flugkoerper-Leitwerks/Antriebs
Proc. of the 1986 American Control Conf. ; 2 ; 1137-1142
1986
6 Seiten, 20 Bilder, 3 Quellen
Aufsatz (Konferenz)
Englisch
New Flutter-Suppression Method for a Missile Fin with an Actuator
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