NASA NTRS · 19670060433
Launch booster gust alleviation.
Abstract
Controller design for booster gust alleviation, considering stochastic minimization problem solved by iteration yielding linear finite time controller with time-varying gains
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Skelton, G. B.. 1967-09-01. Launch booster gust alleviation.. https://ntrs.nasa.gov/citations/19670060433
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