Implementation of Optimal Guidance Laws Using Predicted Missile Velocity Profiles
Author:
Affiliation:
1. Agency for Defense Development, Taejon 305-600, Republic of Korea
2. Korea Advanced Institute of Science and Technology, Taejon 305-701, Republic of Korea
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/10.2514/2.4420
Reference5 articles.
1. Closed-form optimal guidance law for missiles of time-varying velocity
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