A Feedback-Form of Terminal-Phase Optimal Guidance Law for BTT Missiles Considering Autopilot Dynamics
نویسندگان
چکیده
منابع مشابه
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ژورنال
عنوان ژورنال: Journal of the Korean Society for Aeronautical & Space Sciences
سال: 2016
ISSN: 1225-1348
DOI: 10.5139/jksas.2016.44.3.203