Cooperative Guidance for Multiple Powered Missiles with Constrained Impact and Bounded Speed
Author:
Affiliation:
1. Beijing Institute of Technology, 100081 Beijing, People’s Republic of China
2. University of Missouri, Columbia, Missouri 65211
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
Reference39 articles.
1. Impact-time-control guidance law for anti-ship missiles
2. Homing Guidance Law for Cooperative Attack of Multiple Missiles
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5. Nonsingular Sliding Mode Guidance for Impact Time Control
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