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OverviewThe consistently developing abilities of adversary's weapon systems have continued to initiate missile guidance design toward enhanced accuracy, high velocity interception and rapid maneuver capabilities. Both theory and extensive simulation studies indicate that classical guidance and optimal guidance methods cannot guarantee the terminal homing accuracy, which is required against a target with unpredictable maneuvers. This is because these two guidance laws operate on perfect knowledge of target maneuvers. The present work focuses on designing a nonlinear guidance law for missiles against maneuvering targets by utilizing H_∞ control theory. The guidance problem is formulated as a nonlinear disturbance attenuation H_∞ control problem where the target's accelerations are regarded as unpredictable disturbances. In H_∞ guidance law, target acceleration is neither necessary, nor approximated. The objective of the control is to attenuate the influence of the target's maneuvers on guidance law performance. Full Product DetailsAuthor: Makena JacquelinePublisher: LAP Lambert Academic Publishing Imprint: LAP Lambert Academic Publishing Dimensions: Width: 15.20cm , Height: 0.60cm , Length: 22.90cm Weight: 0.159kg ISBN: 9783659713064ISBN 10: 3659713066 Pages: 100 Publication Date: 18 May 2015 Audience: General/trade , General Format: Paperback Publisher's Status: Active Availability: In stock We have confirmation that this item is in stock with the supplier. It will be ordered in for you and dispatched immediately. Table of ContentsReviewsAuthor InformationTab Content 6Author Website:Countries AvailableAll regions |