Control of Impact Time with Increased Robustness via Feedback Linearization
Author:
Affiliation:
1. Aselsan Inc., 06750 Ankara, Turkey
2. Roketsan Missiles Inc., 06780 Ankara, Turkey
3. Technical University of Munich, 85748 Munich, Germany
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
http://arc.aiaa.org/doi/pdf/10.2514/1.G001719
Reference18 articles.
1. Impact-time-control guidance law for anti-ship missiles
2. Impact time control guidance law with field of view constraint
3. Lyapunov-Based Guidance Law for Impact Time Control and Simultaneous Arrival
4. Design of Time-constrained Guidance Laws via Virtual Leader Approach
5. Cooperative Guidance for Multimissile Salvo Attack
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