Stability analysis of spinning missiles induced by seeker disturbance rejection rate parasitical loop-Reference-Cited by-同舟云学术

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Stability analysis of spinning missiles induced by seeker disturbance rejection rate parasitical loop

Published:2019-07 Issue: Volume:90 Page:194-208
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Li Wei,Wen Qiuqiu,Yang Yu

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference40 articles.

1. Coning motion stability of spinning missiles with strapdown seekers;He;Aeronaut. J.,2016

2. Disturbance observer-based control for missile non-strapdown seeker disturbance rejection;Song;Adv. Mech. Eng.,2016

3. Design trade-offs for homing missiles;Spencer,1992

4. Influence of seeker disturbance rejection rate on missile guidance system;Song;J. Harbin Eng. Univ.,2013

5. Guidance Weapon Control Systems;Garnell,2003

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