Aiming point guidance law for air-to-air missiles-Reference-Cited by-同舟云学术

Aiming point guidance law for air-to-air missiles

Published:1998-02 Issue:2 Volume:29 Page:95-102
ISSN:0020-7721
Container-title:International Journal of Systems Science
language:en
Short-container-title:International Journal of Systems Science

Author:

TSAO LU-PING,CHOU CHING-LAIN,CHEN CHUEN-MING,CHEN CHI-TEH

Publisher

Informa UK Limited

Subject

Computer Science Applications,Theoretical Computer Science,Control and Systems Engineering

Link

http://www.tandfonline.com/doi/pdf/10.1080/00207729808929501

Reference8 articles.

1. AL-MASRI , Y. S. , 1986 , Adaptive state estimation compared with proportional navigation for bearing-only missile guidance. PhD thesis, College of Aeronautics , Cranfield Institute of Technology , UK .

2. A new guidance law for homing missiles

3. PATRICK , H. L. , and SELTZER , S. M. , 1979 ,Future US Army missile G&C system.AIAA 79-1974 , pp. 404 – 412 .

4. Guidance Laws for Short-Range Tactical Missiles

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