Guidance Scheme for Gun-Launched Gliding Guided Projectiles

This article 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 homi...

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Vydané v:	IEEE transactions on aerospace and electronic systems Ročník 61; číslo 2; s. 1630 - 1647
Hlavní autori:	Kim, Boseok, Shin, Minjae, Lee, Chang-Hun, Kim, Jin-Won, Lee, Young-Ki, Park, Sung-Woo
Médium:	Journal Article
Jazyk:	English
Vydavateľské údaje:	New York IEEE 01.04.2025 The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Predmet:	Aerodynamic drag Aerodynamics Aerospace and electronic systems Flight Glide paths Gliding Gliding-guided projectiles Gravity gun-launched projectiles Homing Impact angle impact angle constraint maximum-range glide problem Optimal control optimal gliding guidance Optimization Projectiles Tail Trajectory
ISSN:	0018-9251, 1557-9603
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