Guidance Scheme for Gun-Launched Gliding Guided Projectiles

This paper presents a composite guidance approach tailored for gun-launched gliding-guided projectiles. The guidance scheme is designed to maximize the lift-to-drag ratio during the gliding flight phase, thereby extending flight range while adhering to impact angle constraints in the terminal homing...

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Veröffentlicht in:	IEEE transactions on aerospace and electronic systems 2024-09, p.1-17
Hauptverfasser:	Kim, Boseok, Shin, Minjae, Lee, Chang-Hun, Kim, Jin-Won, Lee, Young-Ki, Park, Sung-Woo
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aerospace and electronic systems Gliding-guided projectiles Gravity gun-launched projectiles impact angle constraint maximum-range glide problem Optimal control optimal gliding guidance Projectiles Tail Trajectory
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