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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Veröffentlicht in:	IEEE transactions on aerospace and electronic systems Jg. 61; H. 2; S. 1630 - 1647
Hauptverfasser:	Kim, Boseok, Shin, Minjae, Lee, Chang-Hun, Kim, Jin-Won, Lee, Young-Ki, Park, Sung-Woo
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	New York IEEE 01.04.2025 The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Schlagworte:	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
Online-Zugang:	Volltext
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