Paper is concerned with application of optimal linear-control theory to five-engine flexible rocket booster; paper develops quadratic cost-criterion control law and seeks to approximate required feedback by using multiple-sensor scheme; number of sensors required by proposed scheme is less than order of plant dynamics.
Application of quadratic penalty function criterion to determination of linear control for flexible vehicle
AIAA J
AIAA Journal ; 3 , n 7 ; p 1262-1267
1965
6 pages
Article (Journal)
English
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Optimal Linear-Quadratic Missile Guidance Laws with Penalty on Command Variability
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