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Launch booster gust alleviation.Controller design for booster gust alleviation, considering stochastic minimization problem solved by iteration yielding linear finite time controller with time-varying gains
Document ID
19670060433
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Skelton, G. B.
Date Acquired
August 3, 2013
Publication Date
September 1, 1967
Subject Category
Space Vehicles
Accession Number
67A39162
Funding Number(s)
CONTRACT_GRANT: NAS8-20155
Distribution Limits
Public
Copyright
Other
Keywords
ROCKET BOOSTER
GUST ALLEVIATOR
ITERATIVE SOLUTION
AUTOMATIC CONTROL
GIMBALLED CONTROL

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