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Analytical solutions for extremal space trajectories

Author: Dilmurat M Azimov
Publisher: Oxford, England ; Cambridge, Massachusetts : Butterworth-Heinemann, 2018. ©2018
Edition/Format:   eBook : Document : EnglishView all editions and formats
Summary:
Analytical Solutions for Extremal Space Trajectories presents an overall treatment of the general optimal control problem, in particular, the Mayer's variational problem, with necessary and sufficient conditions of optimality. It also provides a detailed derivation of the analytical solutions of these problems for thrust arcs for the Newtonian, linear central and uniform gravitational fields. These solutions are  Read more...
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Genre/Form: Electronic books
Additional Physical Format: Print version:
Azimov, Dilmurat M.
Analytical solutions for extremal space trajectories.
Oxford, England ; Cambridge, Massachusetts : Butterworth-Heinemann, ©2018
xi, 317 pages
Material Type: Document, Internet resource
Document Type: Internet Resource, Computer File
All Authors / Contributors: Dilmurat M Azimov
ISBN: 9780128140598 0128140593
OCLC Number: 1013852157
Description: 1 online resource (332 pages) : illustrations
Contents: Introduction --
Optimal and exremal trajectories --
Motion with constant power and variable specific impulse --
Motion with variable power and constant specific impulse --
Motion with constant power and constant specific impulse --
Extremal trajectories in a linear central field --
Extremal trajectories in a uniform gravity field --
Number of thrusts arcs for extremal orbital transfers --
Some problems of trajectory synthesis in the Newtonial field --
Conclusions --
Appendix --
Nomenclature --
References --
Index.
Responsibility: Dilmurat M. Azimov.

Abstract:

Analytical Solutions for Extremal Space Trajectories presents an overall treatment of the general optimal control problem, in particular, the Mayer's variational problem, with necessary and sufficient conditions of optimality. It also provides a detailed derivation of the analytical solutions of these problems for thrust arcs for the Newtonian, linear central and uniform gravitational fields. These solutions are then used to analytically synthesize the extremal and optimal trajectories for the design of various orbital transfer and powered descent and landing maneuvers. Many numerical examples utilizing the proposed analytical synthesis of the space trajectories and comparison analyses with numerically integrated solutions are provided. This book will be helpful for engineers and researchers of industrial and government organizations, and is also a great resource for university faculty and graduate and undergraduate students working, specializing or majoring in the fields of aerospace engineering, applied celestial mechanics, and guidance, navigation and control technologies, applied mathematics and analytical dynamics, and avionics software design and development.

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