X射線脈沖星導(dǎo)航：原理與應(yīng)用（英文版）

定　價：￥128.00

作　者：	鄭偉,王奕迪
出版社：	科學(xué)出版社
叢編項：
標(biāo)　簽：	暫缺

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ISBN：	9787030647719	出版時間：	2020-05-01	包裝：
開本：	32開	頁數(shù)：	222	字數(shù)：

內(nèi)容簡介

　　This book discusses autonomous spacecraft navigation based on X-ray pulsars， analyzing how to process X-ray pulsar signals， how to simulate them， and how to estimate the pulse's time of arrival based on epoch folding. In turn， the book presents a range of X-ray pulsar-based spacecraft positioning/time-keeping/attitude determination methods. It also describes the error transmission mechanism of the X-ray pulsar-based navigation system and its corresponding compensation methods. Further， the book introduces readers to navigation based on multiple measurement information fusion， such as X-ray pulsar/traditional celestial body integrated navigation and X- ray pulsar/INS integrated navigation. As such， it offers readers extensive information on both the theory and applications of X-ray pulsar-based navigation， and reflects the latest developments in China and abroad.

作者簡介

暫缺《X射線脈沖星導(dǎo)航：原理與應(yīng)用（英文版）》作者簡介

圖書目錄

1 Introduction
1．1 Basic Concept of Spacecraft Autonomous Navigation
1．1．1 Definition of Spacecraft Autonomous Navigation
1．1．2 Necessity of Autonomous Navigation Systems
1．2 Three Main Types of Spacecraft Autonomous Navigation
1．2．1 Inertial Navigation System
1．2．2 Celestial Navigation System
1．2．3 Navigation Satellite System
1．3 Review of X-Ray Pulsar-Based Navigation
1．3．1 Brief Introduction of Pulsar
1．3．2 Brief Introduction of X-Ray Pulsar-Based Navigation
1．3．3 Famous Programs on XPNAV
1．3．4 Progresses of Key Techniques
2 Fundamential of the X-Ray Pulsar-Based Navigation
2．1 Space-Time Reference Frame
2．1．1 Coordinate System
2．1．2 General Relativistic Time System
2．2．1 Time and Phase Model
2．3 Spacecraft Orbital Dynamics and Attitude Dynamics Models
2．3．1 Spacecraft Orbital Dynamics Model
2．3．2 Spacecraft Attitude Dynamics Model
2．4 X-Ray Pulsar-Based Spacecraft Positioning
2．4．3 Analysis on the X-Ray Detector Configuration
2．5 X-Ray Pulsar-Based Spacecraft Time Keeping
2．5．2 System Equation
2．5．3 Feasibility Analysis of Time-Keeping via the Observation of One Pulsar
2．6 X-Ray Pulsar-Based Spacecraft Attitude Determination
2．6．1 Basic Principle
2．6．2 Means of Realizing Direction via the Observation
References
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3 X-Ray Pulsar Signal Processing
4 Errors Within the Time Transfer Model and Compensation Methods for Earth-Orbing Spacecraft
5 X-Ray Pulsar/Multiple Measurement Information Fused Navigation
6 Spacecraft Autonomous Navigation Using the X-Ray Pulsar Time Difference of Arrival
7 Ground-Based Simulation and Verification System for X-Ray Pulsar-Based Navigation