Cooperative Circular Guidance with Nonuniform Field-of-View Constraints
Author:
Affiliation:
1. Beijing Institute of Technology, 100081 Beijing, People’s Republic of China
2. Beijing Institute of Astronautical Systems Engineering, 100076 Beijing, People’s Republic of China
3. University of Missouri, Columbia, Missouri 65211
Funder
National Natural Science Foundation of China
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.G006470
Reference40 articles.
1. Impact-time-control guidance law for anti-ship missiles
2. Nonsingular Sliding Mode Guidance for Impact Time Control
3. Design of Time-constrained Guidance Laws via Virtual Leader Approach
4. Three-Dimensional Optimal Impact Time Guidance for Antiship Missiles
5. New Differential Geometric Guidance Strategies for Impact-Time Control Problem
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