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Titlebook: Optimal Space Flight Navigation; An Analytical Approa Ashish Tewari Book 2019 Springer Nature Switzerland AG 2019 Orbital Space Mechanics.S

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書目名稱Optimal Space Flight Navigation
副標(biāo)題An Analytical Approa
編輯Ashish Tewari
視頻videohttp://file.papertrans.cn/703/702923/702923.mp4
概述Collects decades of knowledge regarding optimal space flight navigation theory in an accessible manner.Emphasizes an analytical approach to optimal space navigation.Guides readers from basic to advanc
叢書名稱Control Engineering
圖書封面Titlebook: Optimal Space Flight Navigation; An Analytical Approa Ashish Tewari Book 2019 Springer Nature Switzerland AG 2019 Orbital Space Mechanics.S
描述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. Reade
出版日期Book 2019
關(guān)鍵詞Orbital Space Mechanics; Space Flight Navigation; Optimal Control Theory; Optimal Impulsive Guidance; Hi
版次1
doihttps://doi.org/10.1007/978-3-030-03789-5
isbn_ebook978-3-030-03789-5Series ISSN 2373-7719 Series E-ISSN 2373-7727
issn_series 2373-7719
copyrightSpringer Nature Switzerland AG 2019
The information of publication is updating

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Orbital Mechanics and Impulsive Transfer, of the respective bodies are called the orbits. The relative motion of two spherical bodies in mutual gravitational attraction is the fundamental problem of translational space dynamics, called the . (or the .), and possesses an analytical solution.
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Optimal Maneuvers with Bounded Inputs,ded. The trajectory optimization must therefore be performed taking bounded inputs into account. As discussed in the earlier chapters, the nature of optimal trajectories with bounded acceleration inputs can be classified as either impulsive thrust or continuous thrust maneuvers.
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Flight in Non-spherical Gravity Fields,om the flight in the gravity field of a single spherical body, which was covered in the previous chapters. The primary reason for this difference is that the spacecraft is no longer in a time-invariant gravity field of the two-body problem, but instead encounters a time-dependent field due to the re
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Ashish Tewariy estimation problem. The main ideas of our method are to add constraints to enforce landmark correspondences and preserving local neighborhood structure. Landmarks represent the salient points in point sets, which can be computed using feature descriptors such as scale-invariant feature transform.
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Ashish Tewarin establish user profiles through the user’s behavior and other information, and automatically recommend the items that best match the user’s preferences, thus effectively reducing the information overload problem. Although scholars from all over the world have proposed many solutions to the persona
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