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OverviewThe concept of aeroassisting for orbital transfer has been recognised as one of the critical technologies for pioneering the space frontier. In space transportation systems, aeroassisting (or aerobraking), defined as the deceleration resulting from the effects of atmospheric drag upon a vehicle during orbital operations, opens new mission opportunities, especially with regard to the establishment of the permanent Space Station Freedom and space explorations to other planets such as Mars. The main areas of research reported in this monograph are atmospheric entry problems by the method of matched asymptotic expansions, coplanar and non-coplanar orbital transfers with aeroassist technology, orbital plan change with aerocruise, and neighbouring optimal guidance. A special feature is the bibliography which will provide the reader with a literature status for further research. Full Product DetailsAuthor: D.Subbaram NaiduPublisher: Springer-Verlag Berlin and Heidelberg GmbH & Co. KG Imprint: Springer-Verlag Berlin and Heidelberg GmbH & Co. K Volume: 188 Dimensions: Width: 15.50cm , Height: 1.10cm , Length: 23.50cm Weight: 0.335kg ISBN: 9783540198192ISBN 10: 3540198199 Pages: 182 Publication Date: 29 October 1993 Audience: College/higher education , Professional and scholarly , Postgraduate, Research & Scholarly , Professional & Vocational Format: Paperback Publisher's Status: Active Availability: Out of stock  The supplier is temporarily out of stock of this item. It will be ordered for you on backorder and shipped when it becomes available. Table of Contents1. Introduction.- 2. Atmospheric entry problem.- 3. Fuel optimal control for coplanar orbital transfer.- 4. Fuel optimal control for noncoplanar orbital transfer.- 5. Orbital plane change with aerocruise.- 6. Optimal guidance for orbital transfer.ReviewsAuthor InformationTab Content 6Author Website:Countries AvailableAll regions |
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