Time-optimal impact angle control for vertical plane engagements

As a part of trajectory modulation to increase terminal effectiveness, impact angle control is required in the terminal phase of tactical missile systems. Moreover, the missile systems are allowed to have only low altitude and minimum flight time to reduce the probability of detection by sensors of...

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Veröffentlicht in:	IEEE transactions on aerospace and electronic systems 1999-04, Vol.35 (2), p.738-742
Hauptverfasser:	Lyul Song, Taek, Jin Shin, Sang
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aircraft components Automatic pilots Autopilots Control systems Exact solutions Geometry Impact angle Law Mathematical models Missiles Navigation Optimal control Phase modulation Sensor systems Terminals Testing Virtual manufacturing
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