Original paper

Backstepping-Based Impact Time Control Guidance Law for Missiles With Reduced Seeker Field-of-View

Volume: 55, Issue: 1, Pages: 82 - 94
Published: Feb 1, 2019
Abstract
This paper proposes a guidance law that achieves the desired terminal impact time without violating a seeker's field-of-view (FOV) limits. In order to derive the guidance law, kinematic conditions for impact time control are defined, and the backstepping control technique is applied for the satisfaction of the conditions. As a virtual control input for the backstepping structure, the missile lead angle, which represents the angle between the...
Paper Details
Title
Backstepping-Based Impact Time Control Guidance Law for Missiles With Reduced Seeker Field-of-View
Published Date
Feb 1, 2019
Volume
55
Issue
1
Pages
82 - 94
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