Language: English
Published by CreateSpace Independent Publishing Platform, 2014
ISBN 10: 1500903132 ISBN 13: 9781500903138
Seller: GreatBookPrices, Columbia, MD, U.S.A.
Condition: As New. Unread book in perfect condition.
Language: English
Published by CreateSpace Independent Publishing Platform, 2014
ISBN 10: 1500903132 ISBN 13: 9781500903138
Seller: GreatBookPrices, Columbia, MD, U.S.A.
Condition: New.
Language: English
Published by CreateSpace Independent Publishing Platform, 2014
ISBN 10: 1500903132 ISBN 13: 9781500903138
Seller: GreatBookPricesUK, Woodford Green, United Kingdom
Condition: As New. Unread book in perfect condition.
Language: English
Published by CreateSpace Independent Publishing Platform, 2014
ISBN 10: 1500903132 ISBN 13: 9781500903138
Seller: GreatBookPricesUK, Woodford Green, United Kingdom
Condition: New.
Language: English
Published by CreateSpace Independent Publishing Platform, 2014
ISBN 10: 1500903132 ISBN 13: 9781500903138
Seller: California Books, Miami, FL, U.S.A.
Condition: New. Print on Demand.
Condition: Hervorragend. Zustand: Hervorragend | Sprache: Englisch | Produktart: Bücher | Keine Beschreibung verfügbar.
Language: English
Published by Createspace Independent Publishing Platform, 2014
ISBN 10: 1500903132 ISBN 13: 9781500903138
Seller: THE SAINT BOOKSTORE, Southport, United Kingdom
£ 18.22
Quantity: Over 20 available
Add to basketPaperback / softback. Condition: New. This item is printed on demand. New copy - Usually dispatched within 5-9 working days.
Language: English
Published by Createspace Independent Publishing Platform, 2014
ISBN 10: 1500903132 ISBN 13: 9781500903138
Seller: CitiRetail, Stevenage, United Kingdom
Paperback. Condition: new. Paperback. The last several decades have resulted in an unfortunate byproduct of space exploration and development: orbital debris. Satellites in Low Earth Orbit have been required to make an ever increasing number of course corrections in order to avoid collisions. Despite efforts to the contrary, collisions continue to occur, each time creating additional debris and increasing the requirement for the remaining satellites to maneuver. Every required maneuver decreases a satellite's service life. The purpose of this study is to develop a minimum thrust profile to maneuver an orbiting satellite out of its projected error ellipse before a collision occurs. For comparison, both the impulsive and continuous thrust cases were considered as well as in-plane versus out-of plane maneuvering. This study made use of the Radau Pseudospectral Method to develop this minimum thrust profile. This method was run in MATLAB(R) using General Pseudospectral Optimal Control Software (GPOPS-II). Once the optimal solution was obtained, Systems Tool Kit(R) was used to simulate the resulting calculated trajectories and confirm avoidance of the error ellipse. This item is printed on demand. Shipping may be from our UK warehouse or from our Australian or US warehouses, depending on stock availability.