Theory and Design Methods of Special Space Orbits

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Theory and Design Methods of Special Space Orbits

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http://libproxy.rpi.edu/login?url=https://ebookcentral.proquest.com/lib/rpi/detail.action?docID=4751367

Instantiates

• Theory and Design Methods of Special Space Orbits

Publication

• Singapore, Springer, 2016

Copyright

• ©2017

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online resource

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cr

Carrier MARC source

rdacarrier

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multicolored

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text

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txt

Content type MARC source

rdacontent

Contents

• Preface -- Contents -- Abstract -- 1 Overview of Classical Orbits -- 1.1 Recursive Orbit -- 1.1.1 Recursive Orbit: Definition -- 1.1.2 Different Orbital Periods -- 1.1.3 Geostationary Earth Orbit and Its Applications -- 1.2 Sun-Synchronous Orbit -- 1.2.1 Sun-Synchronous Orbit: Definition -- 1.2.2 Sun-Synchronous Orbit: Characteristics -- 1.2.3 Sun-Synchronous Regression Orbit and Its Applications -- 1.3 Frozen Orbit -- 1.3.1 Frozen Orbit: Definition -- 1.3.2 Molniya Orbit and Its Applications -- 1.4 Stay Orbit -- 1.4.1 Stay Orbit: Definition -- 1.4.2 Stay Orbit: Applications -- 1.5 Summary -- 2 Special Space Orbit: Concept and Application -- 2.1 Special Space Orbit: Concept -- 2.1.1 Differences in Orbit Design Concepts -- 2.1.2 Coupling of Orbit Control and Orbit Design -- 2.1.3 Requirements for Special Space Application -- 2.2 Types of Special Orbit -- 2.2.1 Hovering Orbit -- 2.2.2 Cruising Orbit -- 2.2.3 Multi-Target Rendezvous Orbit -- 2.2.4 Initiative Approaching Orbit -- 2.2.5 Fast Responsive Orbit -- 2.2.6 Earth Pole-Sitter Orbit -- 2.3 Description of Special Space Orbit -- 2.3.1 Orbit Element -- 2.3.2 Non Singularity Orbit Elements -- 2.3.3 Rectangular Coordinate Component -- 2.4 Summary -- 3 Theory and Design Method of Hovering Orbit -- 3.1 Hovering Orbit: Concept -- 3.2 Design of Fixed-Point Hovering Orbit -- 3.2.1 Dynamic Model -- 3.2.1.1 Mathematical Model of the Impulse Thrust -- 3.2.1.2 Mathematical Model of Continuous Thrust -- 3.2.1.3 Feasibility Analysis -- 3.2.2 Open-Loop Control -- 3.2.3 Closed Loop Control -- 3.2.3.1 Hovering Control Based on Lyapunov Method -- 3.2.3.2 Simulation Analysis -- 3.3 Design of Regional Hovering Orbit -- 3.3.1 Analysis of Confined Area Configuration -- 3.3.1.1 Description of Confined Area Configuration -- 3.3.1.2 Typical Confined Area Configurations -- 3.3.1.3 Analysis of Confined Area Configuration
• 3.3.2 Control of Regional Hovering Orbit -- 3.3.2.1 Control Model of Relative Motion -- 3.3.2.2 Constraints in Orbit Design -- 3.3.3 Regional Hovering Orbit of Single-Pulse Trust -- 3.3.3.1 Minimum Rate of Energy Consuming Mode -- 3.3.3.2 Fixed Time Mode -- 3.3.4 Regional Hovering Orbit of Multi-Pulse Trust -- 3.4 Design of Displaced Geostationary Orbit -- 3.4.1 Displaced Orbit Deviating from Orbit Plane -- 3.4.2 Displaced Orbit in Orbit Plane -- 3.4.3 Energy Analysis of Orbit Displacement -- 3.5 Summary -- 4 Theory and Design Method of Spiral Cruising Orbit -- 4.1 Spiral Cruising Orbit: Concept -- 4.2 Precision Analysis of Relative Motion Model -- 4.2.1 Accurate Relative Motion Dynamics Equation -- 4.2.2 Simplification of Relative Motion Dynamics Equation -- 4.2.3 Precision Analysis of Relative Motion Dynamics Model -- 4.2.4 Analysis of Relative Motion Dynamics Model of Cruising Spacecraft -- 4.3 Traversal Cruising Orbit: Design -- 4.3.1 Design Method Based on Hill Equation -- 4.3.2 Design Method Based on E/I Vector Method -- 4.3.3 Design Constraint -- 4.3.4 Simulation Analysis -- 4.4 Design of the Round-Trip Itinerant Orbit -- 4.4.1 Design Method -- 4.4.2 Design Constraints -- 4.4.3 Simulation Analysis -- 4.5 Controllable Cruising Orbit: Design -- 4.5.1 Spiral Ring: Design -- 4.5.2 Entry Corridor: Design -- 4.5.3 Single-Pulse Control Strategy -- 4.5.4 Fast Cruising Control Strategy -- 4.6 Summary -- 5 Theory and Design Method of Multi-Target Rendezvous Orbit Based on Traversing Points -- 5.1 Multi-Target Orbital Rendezvous: Problem Description -- 5.2 Traversing Point: Concept and Determination Method -- 5.2.1 Traversing Point: Concept -- 5.2.2 Traversing Point: Determination Method -- 5.3 Orbital Rendezvous: Strategies Based on Traversing Point -- 5.3.1 Design Principles Based on Traversing Point -- 5.3.2 Rendezvous Orbit: Design Method
• 5.3.3 Orbital Rendezvous: Control Method -- 5.4 Non-Coplanar Homogeneous Multi-Target Rendezvous Orbit: Design Method -- 5.5 Non-Coplanar Heterogeneous Multi-Target Rendezvous Orbit: Design Method -- 5.5.1 Design Procedures -- 5.5.2 Rendezvous Orbit: Design Method -- 5.5.3 Traversing Point Set: Determination Method -- 5.5.4 Rendezvous Trajectory: Design Method -- 5.6 Simulation Analysis and Method Correction -- 5.6.1 Simulation of Orbital Rendezvous Based on Traversing Point -- 5.6.2 Method Correction of Orbital Rendezvous Based on Traversing Point -- 5.7 Summary -- 6 Theory and Design Method of Initiative Approaching Orbit -- 6.1 Initiative Approaching Orbit: Concept -- 6.2 Approaching Orbit: Design -- 6.2.1 Phasing Orbit -- 6.2.2 Short-Range Approaching Orbit -- 6.3 Dynamics Model of Relative Position and Attitude -- 6.3.1 Dynamics Model of Relative Attitude -- 6.3.2 Dynamics Model of Relative Position -- 6.4 Ultimate Approaching Orbit: Design -- 6.4.1 The Final Approach for Three-Axis-Stabilized Target Spacecraft -- 6.4.2 Final Approach to the Target Without Attitude Control -- 6.4.3 Simulation and Realization -- 6.5 Summary -- 7 Theory and Design Method of Responsive Orbit -- 7.1 Fast Responsive Orbit: Concept -- 7.2 Circular Fast Flying-Around Orbit -- 7.2.1 Circular Fast Flying-Around Orbit: Design -- 7.2.2 Target Forbidden Zone: Definition -- 7.2.3 Safety Analysis -- 7.3 Fast Access Orbit -- 7.3.1 Low-Earth-Orbit Fast Access Orbit: Design -- 7.3.2 Cobra Orbit: Design -- 7.4 Summary -- 8 Theory and Design Method of Earth Pole-Sitter Orbit -- 8.1 Earth Pole-Sitter Orbit: Concept -- 8.2 Earth Pole-Sitter Orbit: Design Method -- 8.2.1 Dynamic Model in Circular Restricted Three-Body Problem -- 8.2.2 Design of Earth Pole-Sitter Orbit with Fixed Residence Distance -- 8.2.3 Design of Earth Pole-Sitter Orbit with Unfixed Residence Distance
• 8.3 Optimization Design of Earth Pole-Sitter Orbit -- 8.4 Summary -- Appendix A: Optimization Design of Rendezvous Orbit with MATLAB -- References

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1 online resource (248 pages)

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online

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9789811029486

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computer

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rdamedia

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