TOP
0
0
三民出版.新書搶先報|最速、最優惠的新鮮貨報給你知!
地球靜止衛星軌道與共位控制技術(簡體書)
滿額折

地球靜止衛星軌道與共位控制技術(簡體書)

商品資訊

人民幣定價:298 元
定價
:NT$ 1788 元
優惠價
871556
海外經銷商無庫存,到貨日平均30天至45天
下單可得紅利積點:46 點
商品簡介
目次
相關商品

商品簡介

《地球靜止衛星軌道與共位控制技術(英文版)》重點敘述了地球靜止衛星軌道運動及攝動理論;系統介紹了靜止衛星軌道控制理論與方法,以及靜止衛星多星共位控制理論與算法等技術;突出闡述了地球靜止衛星多星共位控制原理及應用。
《地球靜止衛星軌道與共位控制技術(英文版)》注重理論與實踐的結合,力求透徹介紹地球靜止衛星軌道運動、控制原理。

目次

1 Introduction
1.1 General
1.2 The Geostationary Orbit in Math
1.3 The Status of Geostationary Satellites
1.4 The Framework of the Book
References

2 Orbit Motion Foundations
2.1 Introduction
2.2 The Motion of the Earth
2.2.1 A Solar Day
2.2.2 A Sidereal Day
2.2.3 Equinox Direction
2.2.4 Primary Longitude
2.2.5 Local Solar Time
2.2.6 Polar Motion
2.2.7 Precession Motion
2.2.8 Nutation Motion
2.3 Time System
2.3.1 Seconds in a Day
2.3.2 Sidereal Time and Universal Time...
2.3.3 Julian Days and Modified Julian Days
2.3.4 Greenwich Sidereal Time
2.3.5 International Atomic Time
2.3.6 Coordinated Universal Time
2.3.7 Local Time
2.3.8 Ephemeris Time
2.3.9 GPS Time
2.3.10 Time System Summaries
2.4 Reference System
2.4.1 Background and General Definitions
2.4.2 J2000.0 Earth-Centered Inertial System
2.4.3 The Mean Equator and Equinox
2.4.4 The True Equator and Equinox
2.4.5 The Greenwich Meridian-Fixed System
2.4.6 International Terrestrial Reference System
2.4.7 Global Geodetic System
2.4.8 Local Tangential Coordinate System
2.4.9 Orbit RTN Coordinate System
2.4.10 Satellite-Fixed Orbit Coordinate System
2.4.11 Satellite-Fixed East/South/Down Coordinate Frame
2.4.12 Satellite Body Coordinate System
2.5 The Kepler Orbit
2.5.1 Kepler Orbit Elements
2.5.2 The Kepler Orbit with Motion States
2.5.3 The Kepler Orbit with Reference System
2.5.4 The Station Keeping Element
References

3 The Motion of Geostationary Satellite
3.1 Introduction
3.2 The Geostationary Orbit in Inertial Space
3.3 The Geostationary Orbit Relative to the Earth
3.3.1 Linearization of Geocentric Distance
3.3.2 Linearization of the True Anomaly
3.3.3 Linearization of Right Ascension and Longitude
3.3.4 Linearization of Relative Declination
3.4 The Truth of "8"-Shape Subsatellite
3.5 The Relative Motion with Nominal Longitude
3.5.1 The Orbit Motion Projected on the Equator Plane
3.5.2 The Orbit Motion Projected on the Meridian Plane
3.5.3 Relative Motion Projected on the Local Horizontal Plane

4 Geostatlonary Orbit Perturbation
4.1 Introduction
4.2 Natural Evolution Motion Scenery
4.3 Lagrange Equation for Station Keeping Elements
4.3.1 Lagrange Equation for the Drift Vector
4.3.2 Lagrange Equation for the Eccentricity Vector
4.3.3 Lagrange Equation for the Inclination Vector
4.4 The Earth's Non-spherical Perturbation
4.4.1 The Earth's Non-spherical Potential Function
4.4.2 Real Geostationary Orbit
4.4.3 Semi-major Axis Evolution
4.4.4 Longitude Drift Evolution
4.4.5 Mean Longitude Evolution
4.4.6 Inclination Vector Evolution
4.4.7 Eccentricity Vector Evolution
4.5 The Solar and Lunar Perturbation
4.5.1 The Lunar and Solar Potential Function
4.5.2 Semi-major Axis Evolution
4.5.3 Longitude Evolution
4.5.4 Eccentricity Evolution
4.5.5 Inclination Evolution
4.5.6 Solar-Lunar Ephemeris
4.6 The Solar Radiation Perturbation
4.6.1 Solar Radiation Pressure Potential Function.
4.6.2 Longitude Drift Evolution
4.6.3 Eccentricity Evolution
4.6.4 Inclination Evolution
4.6.5 Eclipses of the Solar by the Earth and Moon
4.7 Perturbation Summaries
References

5 Harmonic Analysis Geostationary Orbit
5.1 Introduction
5.2 Harmonic Analysis
5.3 Basic Functions and Periodic Expansion
5.4 Determining the Coefficients with SVD Method
5.5 Longitude and Drift Harmonics
5.6 Eccentricity Vector Harmonics
5.7 Inclination Vector Harmonics
References

6 Correction Geostationary Orbit
6.1 Introduction
6.2 Relative Motion Equation
6.2.1 Radial Equation
6.2.2 Tangential Equation
6.2.3 Normal Equation
6.3 Orbit Correction Equation
6.4 Radial Impulse
6.5 Tangential Impulse
6.6 Normal Impulse
6.7 Continuous Thrust
6.8 Onboard Thrust Configuration

7 Maintaining Geostationary Orbit
7.1 Introduction
7.2 North/South Station Keeping Strategy
7.2.1 General Background
7.2.2 Inclination Dead Band Allocation
7.2.3 Inclination Maneuver Strategy
7.2.4 Maneuver Calculation
7.2.5 Maneuver Planning
7.2.6 Case Study and Simulation
7.3 East/West Station Keeping Strategy
7.3.1 General Background
7.3.2 Longitude Dead Band Allocation
7.3.3 Longitude Maneuver Strategy
7.3.4 Eccentricity Maneuver Strategy
7.3.5 Maneuver Calculation
7.3.6 Single-Pulse Maneuver Planning
7.3.7 Bi-Pulse Maneuver Planning
7.3.8 Tri-Pulse Maneuver Planning
References

8 Collocation Prototypes and Strategies
8.1 Introduction
8.2 Reference and Notation
8.3 Collocation Relative Motion
8.4 Collocation Principles
8.5 Complete Longitude Separation
8.6 Eccentricity Separation
8.6.1 Absolute Eccentricity Offsetting Strategy
8.6.2 Relative Eccentricity Offsetting Strategy
8.6.3 Evaluation of Eccentricity Separation Strategy
8.6.4 Solar Leading Eccentricity Control Strategy..
8.7 Combined Eccentricity and Inclination Separation
8.7.1 The Mathematical Prototype of E/I Strategy..
8.7.2 Inclination Distribution Strategy
8.7.3 Inclination Maintenance Strategy
8.8 A Bi-Satellite E/I Combined Separation Method
8.9 A Coordinated E/I Combined Separation Method
8.10 A Tri-Satellite Hybrid e-i Separation Method
8.11 Safety Analysis and Collision Warning

References

您曾經瀏覽過的商品

購物須知

大陸出版品因裝訂品質及貨運條件與台灣出版品落差甚大,除封面破損、內頁脫落等較嚴重的狀態,其餘商品將正常出貨。

特別提醒:部分書籍附贈之內容(如音頻mp3或影片dvd等)已無實體光碟提供,需以QR CODE 連結至當地網站註冊“並通過驗證程序”,方可下載使用。

無現貨庫存之簡體書,將向海外調貨:
海外有庫存之書籍,等候約45個工作天;
海外無庫存之書籍,平均作業時間約60個工作天,然不保證確定可調到貨,尚請見諒。

為了保護您的權益,「三民網路書店」提供會員七日商品鑑賞期(收到商品為起始日)。

若要辦理退貨,請在商品鑑賞期內寄回,且商品必須是全新狀態與完整包裝(商品、附件、發票、隨貨贈品等)否則恕不接受退貨。

優惠價:87 1556
海外經銷商無庫存,到貨日平均30天至45天

暢銷榜

客服中心

收藏

會員專區