Minimax Attitude Control of Aeroballistic Launch Vehicles
1965
264 pages
Report
Keine Angabe
Englisch
Astronautics , Attitude control , Closed loop system , Flight control , Launch vehicle , Mathematical model , Stability and control , Attitude , Ballistics , Closed , Control , Design , Flight , Launch , Linear , Loop , Mathematics , Minimization , Model , Procedure , Stability , System , Vehicle
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