عنوان

Guidance and control technology of spacecraft on elliptical orbit /

شابک

9789811079597

شابک

9789811079603

شابک

9811079595

شابک

9811079609

شابک اشتباه

9789811079580

شابک اشتباه

9811079587

عنوان اصلي

Guidance and control technology of spacecraft on elliptical orbit /

نام عام مواد

[Book]

نام نخستين پديدآور

Fucheng Liu, Shan Lu, Yue Sun.

محل نشرو پخش و غیره

Singapore :

نام ناشر، پخش کننده و غيره

Springer,

تاریخ نشرو بخش و غیره

[2019]

تاریخ نشرو بخش و غیره

©2019

نام خاص و کميت اثر

1 online resource (xii, 237 pages)

عنوان فروست

Navigation: science and technology

متن يادداشت

Includes bibliographical references.

متن يادداشت

Intro; Preface; Compilation Committee; Contents; 1 Introduction; 1.1 Characteristics of Elliptical Orbit; 1.2 Development of Elliptical Orbit Satellite Application; 1.3 Key Problems in Control System of Elliptical Orbit Spacecraft; 1.4 Structure of This Book; References; 2 Orbit Design of Spacecraft on Elliptical Orbit; 2.1 Introduction; 2.2 Absolute Dynamics Analysis of Elliptical Orbit; 2.2.1 Basic Features of Elliptical Orbit; 2.2.2 Elliptical Orbit Perturbation; 2.3 Autonomous Orbit Prediction of Elliptical Orbit; 2.3.1 Autonomous Orbit Prediction

متن يادداشت

2.3.2 Onboard Orbit Prediction Algorithm of Elliptical Orbit2.3.3 Analysis and Predigestion of Elliptical Orbit Dynamics Model; 2.4 Design of Apogee Rendezvous Orbit; 2.4.1 Drift Characteristics Analysis of Elliptical Orbit; 2.4.2 Design of Frozen Elliptical Orbit; 2.4.3 Design of Little Inclination Elliptical Orbit; 2.5 Elliptical Orbit Rendezvous Method for Inspecting GEO Satellites; References; 3 Formation Configuration Design of Elliptical Orbit; 3.1 Introduction; 3.2 Formation Configuration Design Based on Algebraic Method; 3.2.1 Relative Dynamic Equation; 3.2.2 Relative Periodic Motion

متن يادداشت

3.2.3 Characteristics Analysis of Relative Motion Trajectory3.2.4 Fly-Around Configuration Design; 3.2.5 Accompanying Flying Configuration Design; 3.3 Formation Configuration Design Based on Geometry; 3.3.1 Precise Model of Relative Motion; 3.3.2 First-Order Approximation Model of Relative Motion; 3.3.3 Formation Configuration Design; References; 4 Autonomous Navigation Technology of Whole Space; 4.1 Introduction; 4.2 Common Autonomous Navigation Method of Elliptical Orbit; 4.2.1 Autonomous Navigation Technology of Elliptical Orbit Based on Astronomical Observation

متن يادداشت

4.2.2 Autonomous Navigation Technology of Elliptical Orbit Based on GNSS4.3 Merge Autonomous Navigation Based on SINS/GNSS/CNS; 4.3.1 State Equation of Inertial Navigation; 4.3.2 Observation Equation of SINS/Star Sensor/GNSS Navigation; 4.3.3 Merge Scheme of SINS/Star Sensor/GNSS System; References; 5 Autonomous Navigation Technology of Regional Constellation; 5.1 Introduction; 5.2 Regional Constellation Autonomous Navigation Based on Inter-satellite Ranging; 5.2.1 Constellation Autonomous Navigation System Scheme of Elliptical Orbit

متن يادداشت

5.2.2 High-Precision Orbit Prediction Technology of Constellation Autonomous Navigation System on Elliptical Orbit5.2.3 Technology of Inter-satellite Link Ranging; 5.2.4 Whole Net Filter Scheme of Constellation Autonomous Navigation; 5.3 Rotation Error Estimation of Constellation Configuration Based on Inter-satellite Observation; 5.3.1 Rotation Error Analysis of Region Constellation Autonomous Navigation on Elliptical Orbit; 5.3.2 Rotation Error Mitigation Method Based on Inter-satellite Observation of Constellation Autonomous Navigation on Elliptical Orbit

بدون عنوان

0

بدون عنوان

8

بدون عنوان

8

بدون عنوان

8

بدون عنوان

8

متن يادداشت

This book introduces readers to the navigation, guidance and control technologies involved in single-spacecraft, double-spacecraft, and multiple-spacecraft tasks in elliptical orbits. It comprehensively covers the key technologies of guidance, navigation and control (GNC) system design for spacecraft in elliptical orbits, including the orbit design, formation configuration design and maintenance, autonomous navigation technology and relative navigation technology, as well as autonomous rendezvous technology. The methods that this book introduces are very close to actual practical engineering applications and presented in an accessible style. The book can serve as reference teaching material for senior undergraduates and postgraduates with space navigation related majors, while also providing essential information and guidance for research personnel and engineering technical personnel engaged in the development of GNC systems for spacecraft.

منبع سفارش / آدرس اشتراک

Springer Nature

شماره انبار

com.springer.onix.9789811079597

عنوان

Guidance and control technology of spacecraft on elliptical orbit.

شماره استاندارد بين المللي کتاب و موسيقي

9789811079580

موضوع مستند نشده

Space flight.

موضوع مستند نشده

Space vehicles-- Control systems.

موضوع مستند نشده

Space vehicles-- Orbits.

موضوع مستند نشده

Space flight.

موضوع مستند نشده

Space vehicles-- Control systems.

موضوع مستند نشده

Space vehicles-- Orbits.

موضوع مستند نشده

TECHNOLOGY & ENGINEERING-- Engineering (General)

موضوع مستند نشده

TEC-- 009000

موضوع مستند نشده

TRP

موضوع مستند نشده

TRP

موضوع مستند نشده

TTDS

شماره

ويراست

شماره رده

نشانه اثر

مستند نام اشخاص تاييد نشده

Liu, Fucheng

مستند نام اشخاص تاييد نشده

Lu, Shan

مستند نام اشخاص تاييد نشده

Sun, Yue

تاريخ عمليات

20200823222220.0

قواعد فهرست نويسي ( بخش توصيفي )

pn

نام الکترونيکي

نوع ماده

[Book]

تكميل شده

Y