An Optimal Geometrical Guidance Law for Impact Time and Angle Control

This article proposes an impact time and angle control guidance law based on geometry without estimating the time-to-go. A moving virtual target is artificially placed on the desired collision line, and the missile pursues the virtual target to satisfy the desired impact angle. The moving speed of t...

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Vydané v:	IEEE transactions on aerospace and electronic systems Ročník 59; číslo 6; s. 1 - 10
Hlavní autori:	Hou, Libing, Luo, Haowen, Shi, Heng, Shin, Hyo-Sang, He, Shaoming
Médium:	Journal Article
Jazyk:	English
Vydavateľské údaje:	New York IEEE 01.12.2023 The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Predmet:	Collision dynamics Estimation Geometrical method Heuristic algorithms impact angle control impact time control Missiles Numerical simulation Optimal control optimal guidance Target tracking Terminal guidance Trajectory
ISSN:	0018-9251, 1557-9603
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