Impact Time and Angle Control Based on Constrained Optimal Solutions
Author:
Affiliation:
1. Roketsan Missiles, Inc., 06780 Ankara, Turkey
2. Aselsan, Inc., 06750 Ankara, Turkey
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.G000414
Reference18 articles.
1. Tactical and Strategic Missile Guidance, Sixth Edition
2. Impact-time-control guidance law for anti-ship missiles
3. Impact time control guidance law with field of view constraint
4. Lyapunov-Based Guidance Law for Impact Time Control and Simultaneous Arrival
5. Nonsingular Sliding Mode Guidance for Impact Time Control
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