Abstract We resolve a problem how to control the longitudinal angular motion of flight vehicles (FV) having a system to displace the center of mass in the transverse direction. A structure is determined and a control law is established to start up and shutdown the engines. Formulas to determine the control parameters are obtained.
Control of flight vehicles with the adjustable center of mass
Russian Aeronautics (Iz VUZ) ; 59 , 3 ; 324-330
2016-07-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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