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041 1 _aeng
_hchi
050 4 _aQB355
_b2016 EB
100 1 _aZhang, Yasheng.
245 1 0 _aTheory and design methods of special space orbits
_cYashen Zhang, Yanli Xu, Haijun Zhou
264 1 _aSingapore
_bSpringer
_c2016
300 _a1 recurso en línea (243 páginas)
336 _aTexto
_btxt
_2rdacontent
337 _aelectrónico
_bc
_2rdamedia
338 _arecurso electrónico
_bcr
_2rdacarrier
500 _aSpringerLink
504 _aIncluye referencias bibliográficas
505 0 _aPreface; 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.
505 8 _a2 Special Space Orbit: Concept and Application2.1 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.
505 8 _a3 Theory and Design Method of Hovering Orbit3.1 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.
505 8 _a3.3.1.3 Analysis of Confined Area Configuration3.3.2 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.
505 8 _a4.1 Spiral Cruising Orbit: Concept4.2 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.
588 0 _aVersión impresa
988 _aEBOOK, EBSPRINGER_2017B
650 7 _aÓrbitas
_2embne
_9676092
700 1 _aXu, Yanli.
_eeditor literario
700 1 _aZhou, Haijun.
_eeditor literario
856 4 0 _uhttps://go.openathens.net/redirector/universidadeuropea.es?url=http://link.springer.com/10.1007/978-981-10-2948-6
_zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
942 _2lcc
_cLE
998 _b02/2018
_dz
_e-
_zSI