Midcourse phase guidance of an interceptor: a simplified suboptimal onboard implementation technique

This study deals with the midcourse guidance of an interceptor against various highly maneuvering aerial targets. The interceptors of this class generally use solid propellant-based rocket motors to provide energy for the interceptor to reach the designated target in the specified range. The duratio...

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Vydané v:	Sadhana (Bangalore) Ročník 50; číslo 2; s. 96
Hlavní autori:	Sankar, Ram B, Tiwari, Pawan Kishore, Annam, Chandrakanth, Bandyopadhyay, Bijnan, Arya, Hemendra
Médium:	Journal Article
Jazyk:	English
Vydavateľské údaje:	New Delhi Springer India 08.05.2025 Springer Nature B.V
Predmet:	Aerial targets Aerodynamics Automatic pilots Controllers Degrees of freedom Design Engineering Feedback Interception Interceptors Maneuvering targets Maximization Midcourse guidance Missiles Optimization Rocket engines Solid propellants Velocity Latax autopilot Midcourse guidance Trajectory optimization Optimal guidance Higher-order sliding mode control
ISSN:	0973-7677, 0256-2499, 0973-7677
On-line prístup:	Získať plný text
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