Satellite formation flying : relative dynamics, formation design, fuel optimal maneuvers and formation maintenance
This book systematically describes the concepts and principles for multi-satellite relative motion, passive and near passive formation designs, trajectory planning and control for fuel optimal formation maneuvers, and formation flying maintenance control design. As such, it provides a sound foundati...
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| Main Authors | , , |
|---|---|
| Format | Electronic eBook |
| Language | English |
| Published |
Singapore :
Springer,
2016.
|
| Series | International series on intelligent systems, control and automation--science and engineering ;
v. 87. |
| Subjects | |
| Online Access | Full text |
| ISBN | 9789811023835 9789811023828 |
| Physical Description | 1 online resource : illustrations |
Cover
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| 100 | 1 | |a Wang, Danwei, |e author. | |
| 245 | 1 | 0 | |a Satellite formation flying : |b relative dynamics, formation design, fuel optimal maneuvers and formation maintenance / |c Danwei Wang, Baolin Wu, Eng Kee Poh. |
| 264 | 1 | |a Singapore : |b Springer, |c 2016. | |
| 300 | |a 1 online resource : |b illustrations | ||
| 336 | |a text |b txt |2 rdacontent | ||
| 337 | |a počítač |b c |2 rdamedia | ||
| 338 | |a online zdroj |b cr |2 rdacarrier | ||
| 490 | 1 | |a Intelligent systems, control and automation: Science and engineering ; |v volume 87 | |
| 504 | |a Includes bibliographical references. | ||
| 505 | 0 | |a 1 Introduction; 1.1 Background; 1.1.1 Motivations; 1.1.2 Applications; 1.1.3 Challenges; 1.2 Objectives of This Book; 1.3 Preview of Chapters; References; 2 Dynamic Models of Satellite Relative Motion Around an Oblate Earth; 2.1 Introduction; 2.2 Nonlinear Dynamic Model of Relative Motion; 2.2.1 J2 Reference Satellite Dynamics in LVLH Frame; 2.2.1.1 Properties of LVLH Frame; 2.2.1.2 J2 Dynamics of a Satellite in LVLH Frame; 2.2.2 Derivation of Exact J2 Nonlinear Relative Dynamics; 2.2.2.1 Lagrangian Formulation of Relative Motion; 2.2.2.2 Kinetic Energy; 2.2.2.3 Potential Energy. | |
| 505 | 8 | |a 2.2.2.4 Exact Nonlinear J2 Relative Dynamics2.3 Linearized Dynamic Models of Relative Motion; 2.4 Validation of Proposed Dynamic Models by Simulation; 2.5 Comparison Study of Relative Dynamic Models; 2.5.1 Comparison Method with Model Error Index; 2.5.2 Selected Dynamic Models for Comparison Study; 2.5.2.1 Clohessy-Wiltshire Model; 2.5.2.2 Tschauner-Hempel Model; 2.5.2.3 Unperturbed Nonlinear Model; 2.5.2.4 Schweighart-Sedwick Model; 2.5.2.5 Xu-Wang Model; 2.5.3 Case Studies; 2.5.3.1 Simulation Scenario; 2.5.3.2 Case 1: Error Index Versus Formation Size. | |
| 505 | 8 | |a 2.5.3.3 Case 2: Error Index Versus Eccentricity2.5.3.4 Case 3: Error Index Versus Inclination; 2.5.3.5 Case 4: Error Index Versus Semimajor Axis; 2.6 Summary; References; 3 Passive and Periodic Satellite Formation Design Around an Oblate Earth; 3.1 Introduction; 3.2 Passive and Periodic Relative Motion Under J2 Perturbation; 3.3 Periodic and Quasi-periodic Relative Orbits at Critical Inclination; 3.3.1 Periodic Relative Orbit; 3.3.2 Quasi-periodic Relative Orbit; 3.3.3 Quasi-periodic Relative Orbit Conditions in Terms of Actual Orbit Variables; 3.3.4 Numerical Simulations. | |
| 505 | 8 | |a 3.4 In-Plane Satellite Formation in Eccentric Orbits3.4.1 Identical Anomaly In-Plane Formation; 3.4.2 Differential Anomaly In-Plane Formation; 3.4.3 Almost Constant Separation Formation; 3.5 Conclusions; References; 4 Nonlinear Optimization of Low-Thrust Trajectory for Satellite Formation; 4.1 Introduction; 4.2 Nonlinear Relative Motion Dynamics; 4.3 Problem Formulation of Trajectory Optimization for Satellite Formation; 4.3.1 Initial Condition Constraints; 4.3.2 Final Condition Constraints; 4.3.3 Path Constraints; 4.3.4 Linking Constraints; 4.4 Introduction of Legendre Pseudospectral Method. | |
| 505 | 8 | |a 4.5 Computational Considerations of Nonlinear Programming Problem4.6 Scaling of Nonlinear Programming Problem; 4.6.1 Initial Guess; 4.6.2 Implementation; 4.7 Illustrative Examples; 4.7.1 Example 1: Scenario of Two Satellites, One Burn Phase; 4.7.2 Example 2: Scenario of Two Satellites, Two Phases: Coast-Burn; 4.7.3 Example 3: Scenario of Two Satellites, Three Phases: Burn-Coast-Burn; 4.7.4 Example 4: Scenario of Two Satellites, Four Phases: Coast-Burn-Coast-Burn; 4.7.5 Example 5: Scenario of Formation Reconfiguration Involving Four Satellites. | |
| 506 | |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty | ||
| 520 | |a This book systematically describes the concepts and principles for multi-satellite relative motion, passive and near passive formation designs, trajectory planning and control for fuel optimal formation maneuvers, and formation flying maintenance control design. As such, it provides a sound foundation for researchers and engineers in this field to develop further theories and pursue their implementations. Though satellite formation flying is widely considered to be a major advance in space technology, there are few systematic treatments of the topic in the literature. Addressing that gap, the book offers a valuable resource for academics, researchers, postgraduate students and practitioners in the field of satellite science and engineering. | ||
| 590 | |a SpringerLink |b Springer Complete eBooks | ||
| 650 | 0 | |a Formation flying. | |
| 650 | 0 | |a Automated vehicles. | |
| 650 | 0 | |a Artificial satellites |x Tracking. | |
| 655 | 7 | |a elektronické knihy |7 fd186907 |2 czenas | |
| 655 | 9 | |a electronic books |2 eczenas | |
| 700 | 1 | |a Poh, Eng Kee, |e author. | |
| 700 | 1 | |a Wu, Baolin, |e author. | |
| 776 | 0 | 8 | |i Print version: |t Satellite Formation Flying. |d [Place of publication not identified] : Springer Verlag 2016 |z 9789811023828 |w (OCoLC)953709437 |
| 830 | 0 | |a International series on intelligent systems, control and automation--science and engineering ; |v v. 87. | |
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