Comparison of the Notable Acceleration- and Angle-Based Guidance Laws for a Short-Range Air-to-Surface Missile-Reference-Cited by-同舟云学术

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Comparison of the Notable Acceleration- and Angle-Based Guidance Laws for a Short-Range Air-to-Surface Missile

Published:2011-01 Issue:1 Volume:44 Page:3527-3532
ISSN:1474-6670
Container-title:IFAC Proceedings Volumes
language:en
Short-container-title:IFAC Proceedings Volumes

Author:

Özkan Bülent,Özgören M. Kemal,Mahmutyazicioğlu Gökmen

Publisher

Elsevier BV

Subject

General Medicine

Reference7 articles.

1. Automatic Control of Aircraft and Missiles;Blakelock,1965

2. Modern Navigation, Guidance and Control Processing;Lin,1991

3. Dynamic Modeling, Guidance, and Control of Homing Missiles;Özkan,2005

4. Guidance and Control of Two-part Homing Missiles using the Proportional Navigation Guidance Law;Özkan,2008

5. Implementation of Linear Homing Guidance Law on a Two-part Homing Missile;Özkan,2008

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. Investigation of the Performance Characteristics of the Angle-based Proportional Navigation Guidance Law;European Journal of Science and Technology;2021-10-29

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