Multi-Mode Electric Actuator Dynamic Modelling for Missile Fin Control

Multi-Mode Electric Actuator Dynamic Modelling for Missile Fin Control

Linear first/second order fin direct current (DC) actuator model approximations for missile applications are currently limited to angular position and angular velocity state variables. Furthermore, existing literature with detailed DC motor models is decoupled from the application of interest: tail...

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Bibliographic Details
Main Authors: Bhimashankar Gurav, John Economou, Alistair Saddington, Kevin Knowles
Format: Article
Language:English
Published: MDPI AG 2017-06-01
Series:Aerospace
Subjects:
actuator
aerodynamic load torque
feedforward
compensation
missile
position control
Online Access:http://www.mdpi.com/2226-4310/4/2/30

Internet

http://www.mdpi.com/2226-4310/4/2/30

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