Impact-Angle-Constrained Cooperative Guidance for Salvo Attack
Author:
Affiliation:
1. Beijing Institute of Technology, 100081 Beijing, People’s Republic of China
2. University of Missouri, Columbia, Missouri 65211
Funder
National Natural Science Foundation of China
China Scholarship Council
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.G006342
Reference46 articles.
1. Tactical and Strategic Missile Guidance, Sixth Edition
2. Terminal Guidance for Impact Attitude Angle Constrained Flight Trajectories
3. Biased PNG law for impact with angular constraint
4. Optimal Guidance Laws with Terminal Impact Angle Constraint
5. Time-to-go weighted optimal guidance with impact angle constraints
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