当前位置：
首页
>
电子教材
>
详细信息
快速检索
数据库：
各中心已购纸本教材
各中心已购电子教材
国内高校课程
国外著名大学课程
外文原版教材出版信息
外文影印版教材出版信息
名校购书信息
关键词：
Spacecraft Dynamics and Control - an Introduction
书目信息
ISBN：
9781118342367
本馆索书号：
中图分类号：
V4
中文译名：
作者：
Anton de Ruiter
编者：
语种：
英语
出版信息
出版社：
Wiley
出版地：
出版年：
2013
版本：
版本类型：
原版
丛书题名：
卷期：
文献信息
关键词：
前言：
摘要：
Provides the basics of spacecraft orbital dynamics plus attitude dynamics and control, using vectrix notation Spacecraft Dynamics and Control: An Introduction presents the fundamentals of classical control in the context of spacecraft attitude control. This approach is particularly beneficial for the training of students in both of the subjects of classical control as well as its application to spacecraft attitude control. By using a physical system (a spacecraft) that the reader can visualize (rather than arbitrary transfer functions), it is easier to grasp the motivation for why topics in control theory are important, as well as the theory behind them. The entire treatment of both orbital and attitude dynamics makes use of vectrix notation, which is a tool that allows the user to write down any vector equation of motion without consideration of a reference frame. This is particularly suited to the treatment of multiple reference frames. Vectrix notation also makes a very clear distinction between a physical vector and its coordinate representation in a reference frame.; This is very important in spacecraft dynamics and control problems, where often multiple coordinate representations are used (in different reference frames) for the same physical vector.
内容简介：
目次：
全文链接：
http://www.itextbook.cn/f/book/bookDetail?bookId=8356b5e1efb74b3ca2a753e759db85e1
读者对象：
实体信息
页码：
其它信息
原版ISBN：
书评：
扩展信息
相关附件