Miss distance dynamics in homing missiles

Author:

NESLINE F.1,ZARCHAN P.1

Affiliation:

1. Raytheon Co., System Design Laboratory, Bedford, MA

Publisher

American Institute of Aeronautics and Astronautics

Cited by 9 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Bounds on the Miss of Radar-Guided Missiles with Discrete Guidance;Journal of Guidance, Control, and Dynamics;2020-04

2. History-dependent modified sliding mode interception strategies with maximal capture zone;Journal of the Franklin Institute;2012-03

3. Seeker Based Optimal Guidance Law, A Few Issues;AIAA Guidance, Navigation, and Control Conference and Exhibit;2003-06-22

4. Integrated terminal guidance and automatic pilot using subspace-stabilization;AIAA Guidance, Navigation, and Control Conference and Exhibit;2001-08-06

5. Normalized analysis of interceptor missiles using the 4-state optimal guidance system;AIAA Guidance, Navigation, and Control Conference and Exhibit;2001-08-06

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