Dynamic stability conditions for a rolling flight vehicle applying continuous actuator-Reference-Cited by-同舟云学术

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Dynamic stability conditions for a rolling flight vehicle applying continuous actuator

Published:2015-04 Issue: Volume:42 Page:451-458
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Koohmaskan Yousof,Arvan Mohammad Reza,Vali Ahmad Reza,Behazin Farid

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference33 articles.

1. Automatic Control of Aircraft and Missiles;Blakelock,1991

2. Linear Matrix Inequalities in System and Control Theory;Boyd,1994

3. Ballistics: Theory and Design of Guns and Ammunition;Carlucci,2007

4. Attitude guidance for spinning vehicle with independent pitch and yaw control;Creagh;J. Guid. Control Dyn.,2010

5. Modern Control Systems;Dorf,2008

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