Sliding-Mode Impact Time Guidance Law Design for Various Target Motions
Author:
Affiliation:
1. Beihang University, 100191 Beijing, People’s Republic of China
2. University of Missouri, Columbia, Missouri 65211-2200
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.G003620
Reference42 articles.
1. Tactical and Strategic Missile Guidance, Sixth Edition
2. A New Look at Classical vs Modern Homing Missile Guidance
3. Optimality of Proportional Navigation Based on Nonlinear Formulation
4. Impact Angle Control Based on Feedback Linearization
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