Closed-form analytical solutions are found which relate various parameters in off-on control systems; relationship is shown among lead time, rise time, delay time, dwell time, and limit-cycle amplitude determined as functions of inertia, aerodynamic damping, and available control moment; application to boost-glide vehicles.
Closed-loop flip-flop control systems
J Aerospace Sciences
Journal of Aerospace Sciences ; 27 , n 11
1960
13 pages
Aufsatz (Zeitschrift)
Englisch
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