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; techniques for interpreting solutions to problems in terms of multiple phase plane plots are given.
Optimal control of maneuver-induced vibration in flexible aerospace vehicles
AIAA J
AIAA Journal ; 5 , n 11
1967
4 pages
Article (Journal)
English
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Optimal control of maneuver-induced vibration in flexible aerospace vehicles
Engineering Index Backfile | 1967
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