ADVANCED INTERCEPTOR AUTOPILOT DESIGN VIA SLIDING MODE CONTROL

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" ADVANCED INTERCEPTOR AUTOPILOT DESIGN VIA SLIDING MODE CONTROL "

Document Type	:	Latin Dissertation
Language of Document	:	English
Record Number	:	151278
Doc. No	:	ET23070
Main Entry	:	RICHARD FRANKLIN TOOMEY
Title Proper	:	ADVANCED INTERCEPTOR AUTOPILOT DESIGN VIA SLIDING MODE CONTROL
Note	:	This document is digital این مدرک بصورت الکترونیکی می باشد
Abstract	:	In this work. a robust tactical missile autopilot for roll stabilization and lateralacceleration tracking is designed via sliding mode control. A nonlinear uncertain model ofthe missile's dynamics is used. Roll stabilization is achieved using a multiple time scalesliding mode controller, resulting in decoupled pitch and yaw motion. Lateral accelerationtracking is achieved using two methods. The first method utilizes a multiple time scalesliding mode controller when the internal dynamics of the missile are stable. The second.-....,....-...,..tested for theQ1 PC1 bus cardBoth these projects mere sofixare des elopment efforts tonards contributing to dlfferentaspects of Roboucs and lZ1echatronics projects m the Controls and Roboucs Group..
Subject	:	Electericl tess
	:	برق
electronic file name	:	TL46304.pdf
Title and statement of responsibility and	:	ADVANCED INTERCEPTOR AUTOPILOT DESIGN VIA SLIDING MODE CONTROL [Thesis]