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On characteristic modeling of a class of flight vehicles’ attitude dynamics

✍ Scribed by Bin Meng; HongXin Wu


Book ID
107356639
Publisher
SP Science China Press
Year
2010
Tongue
English
Weight
611 KB
Volume
53
Category
Article
ISSN
1006-9321

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The influence of structure modal parameters on the dynamics of an integrated actuator and control surface system is studied in this paper. The control surface is modeled as a uniform thickness plate mounted on a push-pull hydraulic actuator. The transfer function between the command and measurement