A Feedback-Form of Terminal-Phase Optimal Guidance Law for BTT Missiles Considering Autopilot Dynamics
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Published:2016-03-01
Issue:3
Volume:44
Page:203-211
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ISSN:1225-1348
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Container-title:Journal of the Korean Society for Aeronautical & Space Sciences
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language:en
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Short-container-title:Journal of the Korean Society for Aeronautical & Space Sciences
Author:
Yoo Seong-Jae,Hong Jin-Woo,Ha In-Joong
Publisher
The Korean Society for Aeronautical & Space Sciences