Evaluation and selection of missile's optimal initial launch azimuth under side window detection using a hybrid decision making method-Reference-Cited by-同舟云学术

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Evaluation and selection of missile's optimal initial launch azimuth under side window detection using a hybrid decision making method

Published:2018-05 Issue: Volume:76 Page:217-228
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Yu Ying,Hou Mingshan,Liu Bojun

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference23 articles.

1. Attitude variable structure control for side window detection;Zhou;Mod. Def. Technol.,2006

2. Digital simulation of kinetic kill vehicle with side window operating in higher atmosphere;Zhang;J. Syst. Simul.,2007

3. Control and guide system design method for side window detection;Song;Mod. Def. Technol.,2007

4. Designing variable structure guidance law for side window detection;Ge;Mod. Def. Technol.,2008

5. Variable structure bang–bang attitude control for space interception using side window detection;Ge;J. Project. Rockets Missiles Guid.,2010

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