Impact Angle Control Guidance under Field-of-View Limitations Based on an Initial-State-Dependent Sliding Surface-Reference-Cited by-同舟云学术

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Impact Angle Control Guidance under Field-of-View Limitations Based on an Initial-State-Dependent Sliding Surface

Published:2022-01-03 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2022 Forum
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Author:

Kikukawa Yuhei¹,Yamasaki Takeshi¹,Takano Hiroyuki¹,Yamaguchi Isao¹

Affiliation:

1. Boei Daigakko

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-2037

Reference21 articles.

1. Zarchan, P., Tactical and Strategic Missile Guidance -SixthEdition- ch.2, pp.13, AIAA, 2007.

2. Guidance of Unmanned Aerial Vehicles

3. Proportional Navigation: Optimal Homing and Optimal Evasion

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