Limitations of autopilot design for controlling a statically unstable flexible interceptor

The Mach number, angle of attack and altitude of operation for an interceptor vary widely during the course of its trajectory. As a result, the interceptor Center of Pressure (CP) locations move significantly around a given Center of Gravity (CG) location at these operating conditions. This results...

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Veröffentlicht in:	Journal of the Franklin Institute 2021-08, Vol.358 (12), p.6121-6135
Hauptverfasser:	Sankar, Ram B., Tiwari, Pawan Kishore, Bandyopadhyay, Bijnan, Arya, Hemendra
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamic configurations Aerodynamic stability Aerodynamics Angle of attack Automatic pilots Bearings Center of gravity Center of pressure Configuration management Control stability Design Flexibility Gravity Mach number Static stability Studies Vibration
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