Missile Guidance Law Considering Constraints on Impact Angle and Terminal Angle of Attack-Reference-Cited by-同舟云学术

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Missile Guidance Law Considering Constraints on Impact Angle and Terminal Angle of Attack

Published:2015-01-02 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference
language:
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Author:

Kim Hyeonggeun¹,Kim H Jin¹

Affiliation:

1. Seoul National University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-0861

Reference17 articles.

1. Terminal Guidance for Impact Attitude Angle Constrained Flight Trajectories

2. Biased PNG law for impact with angular constraint

3. Optimal Guidance Laws with Terminal Impact Angle Constraint

4. Impact Angle Constrained Interception of Stationary Targets

Cited by 1 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. Trajectory Shaping Guidance Law Based on Downrange-to-Go Polynomial;Advances in Aerospace Guidance, Navigation and Control;2017-12-15

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