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Applied Nonsingular Astrodynamics: Optimal Low-Thrust Orbit Transfer (Cambridge Aerospace Series, Series Number 45) - Hardcover
Synopsis
This essential book describes the mathematical formulations and subsequent computer simulations required to accurately project the trajectory of spacecraft and rockets in space, using the formalism of optimal control for minimum-time transfer in general elliptic orbit. The material will aid research students in aerospace engineering, as well as practitioners in the field of spaceflight dynamics, in developing simulation software to carry out trade studies useful in vehicle and mission design. It will teach readers to develop flight software for operational applications in autonomous mode, so to actually transfer space vehicles from one orbit to another. The practical, real-life applications discussed will give readers a clear understanding of the mathematics of orbit transfer, allow them to develop their own operational software to fly missions, and to use the contents as a research tool to carry out even more complex analyses.
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Book Description
This unique book provides readers with a clear understanding of the mathematics of orbit transfer while allowing them to develop their own operational software to fly actual missions, and to use the contents as a research tool to carry out even more complex analyses. It also covers a number of practical, real-life applications.
About the Author
Jean Albert Kéchichian is a retired Engineering Specialist from The Aerospace Corporation. His career has included senior level engineering positions at NASA's Jet Propulsion Laboratory and at Ford Aerospace. His main areas of contribution are in spaceflight guidance and navigation. He is a Fellow of The American Astronautical Society, and his work has regularly appeared in Acta Astronautica, the Journal of Guidance Control and Dynamics, the Journal of the Astronautical Sciences, and the Journal of Spacecraft and Rockets. He holds Degrees in Aeronautical and Mechanical Engineering from l'Université de Ličge, University of California, Berkeley, and a Ph.D. in Aeronautics and Astronautics from Stanford University.
"About this title" may belong to another edition of this title.
- PublisherCambridge University Press
- Publication date2018
- ISBN 10 1108472362
- ISBN 13 9781108472364
- BindingHardcover
- LanguageEnglish
- Edition number1
- Number of pages476
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APPLIED NONSINGULAR ASTRODYNAMICS
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Applied Nonsingular Astrodynamics: Optimal Low-Thrust Orbit Transfer (Cambridge Aerospace Series)
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Applied Nonsingular Astrodynamics: Optimal Low-Thrust Orbit Transfer (Cambridge Aerospace Series, Series Number 45)
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Applied Nonsingular Astrodynamics
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Applied Nonsingular Astrodynamics (Hardcover)
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ISBN 10: 1108472362
ISBN 13: 9781108472364
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Hardcover. Condition: new. Hardcover. This essential book describes the mathematical formulations and subsequent computer simulations required to accurately project the trajectory of spacecraft and rockets in space, using the formalism of optimal control for minimum-time transfer in general elliptic orbit. The material will aid research students in aerospace engineering, as well as practitioners in the field of spaceflight dynamics, in developing simulation software to carry out trade studies useful in vehicle and mission design. It will teach readers to develop flight software for operational applications in autonomous mode, so to actually transfer space vehicles from one orbit to another. The practical, real-life applications discussed will give readers a clear understanding of the mathematics of orbit transfer, allow them to develop their own operational software to fly missions, and to use the contents as a research tool to carry out even more complex analyses. This unique book provides readers with a clear understanding of the mathematics of orbit transfer while allowing them to develop their own operational software to fly actual missions, and to use the contents as a research tool to carry out even more complex analyses. It also covers a number of practical, real-life applications. Shipping may be from multiple locations in the US or from the UK, depending on stock availability. Seller Inventory # 9781108472364
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Applied Nonsingular Astrodynamics: Optimal Low-thrust Orbit Transfer
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Applied Nonsingular Astrodynamics (Hardcover)
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ISBN 10: 1108472362
ISBN 13: 9781108472364
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Hardcover. Condition: new. Hardcover. This essential book describes the mathematical formulations and subsequent computer simulations required to accurately project the trajectory of spacecraft and rockets in space, using the formalism of optimal control for minimum-time transfer in general elliptic orbit. The material will aid research students in aerospace engineering, as well as practitioners in the field of spaceflight dynamics, in developing simulation software to carry out trade studies useful in vehicle and mission design. It will teach readers to develop flight software for operational applications in autonomous mode, so to actually transfer space vehicles from one orbit to another. The practical, real-life applications discussed will give readers a clear understanding of the mathematics of orbit transfer, allow them to develop their own operational software to fly missions, and to use the contents as a research tool to carry out even more complex analyses. This unique book provides readers with a clear understanding of the mathematics of orbit transfer while allowing them to develop their own operational software to fly actual missions, and to use the contents as a research tool to carry out even more complex analyses. It also covers a number of practical, real-life applications. Shipping may be from our UK warehouse or from our Australian or US warehouses, depending on stock availability. Seller Inventory # 9781108472364
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Applied Nonsingular Astrodynamics (Hardcover)
Published by
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ISBN 10: 1108472362
ISBN 13: 9781108472364
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Hardcover
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Hardcover. Condition: new. Hardcover. This essential book describes the mathematical formulations and subsequent computer simulations required to accurately project the trajectory of spacecraft and rockets in space, using the formalism of optimal control for minimum-time transfer in general elliptic orbit. The material will aid research students in aerospace engineering, as well as practitioners in the field of spaceflight dynamics, in developing simulation software to carry out trade studies useful in vehicle and mission design. It will teach readers to develop flight software for operational applications in autonomous mode, so to actually transfer space vehicles from one orbit to another. The practical, real-life applications discussed will give readers a clear understanding of the mathematics of orbit transfer, allow them to develop their own operational software to fly missions, and to use the contents as a research tool to carry out even more complex analyses. This unique book provides readers with a clear understanding of the mathematics of orbit transfer while allowing them to develop their own operational software to fly actual missions, and to use the contents as a research tool to carry out even more complex analyses. It also covers a number of practical, real-life applications. Shipping may be from our Sydney, NSW warehouse or from our UK or US warehouse, depending on stock availability. Seller Inventory # 9781108472364
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