Title :
Control of spinning flying vehicles utilizing partial body despin techniques
Author :
Salman, Mishah Uzziél ; Chang, Borchin ; Ilg, Mark Dean
Author_Institution :
Dept. of Mech. Eng., Drexel Univ., Philadelphia, PA, USA
Abstract :
Despinning the front end of a spinning flying munition is an important step towards flight control of said vehicle. A counter-rotation control scheme is proposed to despin and stabilize the front end of the vehicle at a definable still roll position with respect to earth. Classical and Hinfin control theories are employed to construct the despin controller.
Keywords :
Hinfin control; aircraft control; military systems; missile control; stability; Hinfin control; counter-rotation control scheme; flight control; missile control; partial body despin technique; roll position; spinning flying munition vehicle control; stabilization; Actuators; Aerodynamics; Control systems; Earth; Frequency; Missiles; Space technology; Spinning; Vehicle dynamics; Weapons;
Conference_Titel :
Asian Control Conference, 2009. ASCC 2009. 7th
Conference_Location :
Hong Kong
Print_ISBN :
978-89-956056-2-2
Electronic_ISBN :
978-89-956056-9-1
