Forces applied to large aerospace vehicle to change attitude or velocity of vehicle will often excite significant undesirable vibration; some typical thrust patterns are examined which accomplish desired maneuver and also are constrained to leave some vibratory modes unexcited at conclusion of maneuver; added cost in terms of time for maneuver, complexity of thrust pattern, and fuel or total control effort is examined for optimal maneuvers of this type; techniques for interpreting solutions to these problems in terms of multiple phase plane plots are given.
Optimal control of maneuver-induced vibration in flexible aerospace vehicles
AIAA/ASME -- Tech Paper
Meeting of the 8th AIAA/ASME -- Structures, Structural Dynamics and Materials Conference ; 1967 Vibrations
1967
6 pages
Conference paper
English
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Optimal control of maneuver-induced vibration in flexible aerospace vehicles
Engineering Index Backfile | 1967
|Neural optimal control of flexible spacecraft slew maneuver
Online Contents | 2004
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