Field-of-View Constrained Three-Dimensional Impact Angle Control Guidance for Speed-Varying Missiles

This article develops a three-dimensional (3-D) impact angle control guidance law with the field-of-view (FOV) constraint. The impact error is defined as the difference between the predicted impact angle by proportional navigation guidance and the desired impact angle. The derived guidance command e...

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Veröffentlicht in:	IEEE transactions on aerospace and electronic systems Jg. 58; H. 5; S. 3992 - 4003
Hauptverfasser:	Wang, Jianan, Ding, Xiangjun, Chen, Yadong, Wang, Chunyan, Xin, Ming
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	New York IEEE 01.10.2022 The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Schlagworte:	3-D guidance Constraints Convergence Errors Field of view Field-of-view (FOV) constraint Guidance (motion) Guided missiles Impact angle impact angle control Impact prediction Interception Kinematics Lead Missile control Missiles Numerical simulation Proportional navigation Quaternions Terminal guidance time-varying speed Trajectories Trajectory
ISSN:	0018-9251, 1557-9603
Online-Zugang:	Volltext
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