New Differential Geometric Guidance Strategies for Impact-Time Control Problem
Author:
Affiliation:
1. Harbin Institute of Technology, 150001 Harbin, People’s Republic of China
2. Iowa State University, Ames, Iowa 50010-2271
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
Reference37 articles.
1. Impact-time-control guidance law for anti-ship missiles
2. Impact-Time-Control Guidance with Generalized Proportional Navigation Based on Nonlinear Formulation
3. Homing Guidance Law for Cooperative Attack of Multiple Missiles
4. Nonsingular Sliding Mode Guidance for Impact Time Control
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