Author:
QI Naiming,LIU Yanfang,SUN Xiaolei
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Reference14 articles.
1. 1) Zarchan, P.: Tactical and Strategic Missile Guidance, Progress in Astronautics and Aeronautics Series, Vol. 157, AIAA Inc., Washington, DC, 1994, pp. 25–42.
2. Optimum intercept laws for accelerating targets.
3. Proportional Navigation Miss Distance in the Presence of Bounded Inputs
4. Nonorthodox Guidance Law Development Approach for Intercepting Maneuvering Targets
5. 5) Shinar, J., Shima, T. and Kebke, A.: On the Validity of Linearized Analysis in the Interception of Reentry Vehicles, Proceedings of the AIAA Guidance, Navigation, and Control Conference, AIAA, Reston, VA, 1998, pp. 1050–1060.
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