Explicit Guidance of Ballistic Entry Using Improved Matched Asymptotic Expansions
Author:
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/50/168/50_168_121/_pdf
Reference16 articles.
1. 1) Zarchan, P.: Tactical and Strategic Missile Guidance, 2nd ed., AIAA Progress Series, Vol. 157, AIAA, Washington, D.C., 1994.
2. Improved matched asymptotic solutions for deceleration control during atmospheric entry
3. China’s missile tests in the Taiwan Strait
4. Near-Optimal Guidance Law for Ballistic Missile Interception
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