用户名  找回密码
 To register

QQ登录

只需一步,快速开始

扫一扫,访问微社区

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

[复制链接]
查看: 39620|回复: 36
发表于 2025-3-21 16:12:23 | 显示全部楼层 |阅读模式
书目名称Optimal Space Flight Navigation
副标题An Analytical Approa
编辑Ashish Tewari
视频video
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
丛书名称Control Engineering
图书封面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
关键词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

书目名称Optimal Space Flight Navigation影响因子(影响力)




书目名称Optimal Space Flight Navigation影响因子(影响力)学科排名




书目名称Optimal Space Flight Navigation网络公开度




书目名称Optimal Space Flight Navigation网络公开度学科排名




书目名称Optimal Space Flight Navigation被引频次




书目名称Optimal Space Flight Navigation被引频次学科排名




书目名称Optimal Space Flight Navigation年度引用




书目名称Optimal Space Flight Navigation年度引用学科排名




书目名称Optimal Space Flight Navigation读者反馈




书目名称Optimal Space Flight Navigation读者反馈学科排名




单选投票, 共有 1 人参与投票
 

0票 0.00%

Perfect with Aesthetics

 

0票 0.00%

Better Implies Difficulty

 

1票 100.00%

Good and Satisfactory

 

0票 0.00%

Adverse Performance

 

0票 0.00%

Disdainful Garbage

您所在的用户组没有投票权限
发表于 2025-3-21 23:31:02 | 显示全部楼层
发表于 2025-3-22 01:05:50 | 显示全部楼层
发表于 2025-3-22 04:57:13 | 显示全部楼层
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.
发表于 2025-3-22 10:41:35 | 显示全部楼层
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.
发表于 2025-3-22 15:20:02 | 显示全部楼层
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
发表于 2025-3-22 19:10:02 | 显示全部楼层
发表于 2025-3-23 00:35:16 | 显示全部楼层
发表于 2025-3-23 04:34:20 | 显示全部楼层
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.
发表于 2025-3-23 09:12:18 | 显示全部楼层
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
 关于派博传思  派博传思旗下网站  友情链接
派博传思介绍 公司地理位置 论文服务流程 影响因子官网 SITEMAP 大讲堂 北京大学 Oxford Uni. Harvard Uni.
发展历史沿革 期刊点评 投稿经验总结 SCIENCEGARD IMPACTFACTOR 派博系数 清华大学 Yale Uni. Stanford Uni.
|Archiver|手机版|小黑屋| 派博传思国际 ( 京公网安备110108008328) GMT+8, 2025-5-17 02:26
Copyright © 2001-2015 派博传思   京公网安备110108008328 版权所有 All rights reserved
快速回复 返回顶部 返回列表