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Optimal space flight navigation = an...

Tewari, Ashish.

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Optimal space flight navigation = an analytical approach /

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Optimal space flight navigation/ by Ashish Tewari.
其他題名:	an analytical approach /
作者:	Tewari, Ashish.
出版者:	Cham :Springer International Publishing : : 2019.,
面頁冊數:	xi, 270 p. :ill., digital ;24 cm.
內容註:	1. Introduction -- 2. Analytical Optimal Control -- 3. Orbital Mechanics and Impulsive Transfer -- 4. Two-Body Maneuvers with Unbounded Continuous Inputs -- 5. Optimal Maneuvers with Bounded Inputs -- 6. Flight in Non-spherical Gravity Fields.
Contained By:	Springer eBooks
標題:	Navigation (Astronautics) -
電子資源:	https://doi.org/10.1007/978-3-030-03789-5
ISBN:	9783030037895

Optimal space flight navigation = an analytical approach /
Tewari, Ashish.

Optimal space flight navigationan analytical approach /[electronic resource] :by Ashish Tewari. - Cham :Springer International Publishing :2019. - xi, 270 p. :ill., digital ;24 cm. - Control engineering,2373-7719. - Control engineering..

1. Introduction -- 2. Analytical Optimal Control -- 3. Orbital Mechanics and Impulsive Transfer -- 4. Two-Body Maneuvers with Unbounded Continuous Inputs -- 5. Optimal Maneuvers with Bounded Inputs -- 6. Flight in Non-spherical Gravity Fields.

This book consolidates decades of knowledge on space flight navigation theory, which has thus far been spread across various research articles. By gathering this research into a single text, it will be more accessible to students curious about the study of space flight navigation. Books on optimal control theory and orbital mechanics have not adequately explored the field of space flight navigation theory until this point. The opening chapters introduce essential concepts within optimal control theory, such as the optimization of static systems, special boundary conditions, and dynamic equality constraints. An analytical approach is focused on throughout, as opposed to computational. The result is a book that emphasizes simplicity and practicability, which makes it accessible and engaging. This holds true in later chapters that involve orbital mechanics, two-body maneuvers, bounded inputs, and flight in non-spherical gravity fields. The intended audience is primarily upper-undergraduate students, graduate students, and researchers of aerospace, mechanical, and/or electrical engineering. It will be especially valuable to those with interests in spacecraft dynamics and control. Readers should be familiar with basic dynamics and modern control theory. Additionally, a knowledge of linear algebra, variational methods, and ordinary differential equations is recommended.

ISBN: 9783030037895

Standard No.: 10.1007/978-3-030-03789-5doiSubjects--Topical Terms:

1532757
Navigation (Astronautics)

LC Class. No.: TL1065 / .T493 2019

Dewey Class. No.: 629.4742

Optimal space flight navigation = an analytical approach /
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520 $a This book consolidates decades of knowledge on space flight navigation theory, which has thus far been spread across various research articles. By gathering this research into a single text, it will be more accessible to students curious about the study of space flight navigation. Books on optimal control theory and orbital mechanics have not adequately explored the field of space flight navigation theory until this point. The opening chapters introduce essential concepts within optimal control theory, such as the optimization of static systems, special boundary conditions, and dynamic equality constraints. An analytical approach is focused on throughout, as opposed to computational. The result is a book that emphasizes simplicity and practicability, which makes it accessible and engaging. This holds true in later chapters that involve orbital mechanics, two-body maneuvers, bounded inputs, and flight in non-spherical gravity fields. The intended audience is primarily upper-undergraduate students, graduate students, and researchers of aerospace, mechanical, and/or electrical engineering. It will be especially valuable to those with interests in spacecraft dynamics and control. Readers should be familiar with basic dynamics and modern control theory. Additionally, a knowledge of linear algebra, variational methods, and ordinary differential equations is recommended.
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