On-line pulse control for vibration suppression in a flexible spacecraft was evaluated. A continuous beam vs. a truss was modeled. A linear finite element model was used to determine the truss characteristics. Control issues outlined are ED pulse actuator development, pseudo pulse algorithm development, and large nonlinear simulation problems

Bekey, G. A.

Masri, S. F.

Miller, R. K.

English

NASA Technical Reports Server

N87=17834 :
Evaluation of On-Line
Pulse Control for
V ibration Suppress ion
in Flexible Spacecraft
by
G=
S°
A. Bekey
F. Masri
R. K. Miller
Univ. of So. California
337
https://ntrs.nasa.gov/search.jsp?R=19870008401 2020-03-20T12:42:54+00:00Z
EVALUAT/ON OF ON-I. IN£
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Evaluation of on-line pulse control for vibration suppression in flexible spacecraft

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