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|a GWRE
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|a TL1050
|b .W45 2010
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1 |
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|a Weiland, Claus.
|0 http://id.loc.gov/authorities/names/n79024127
|1 http://isni.org/isni/0000000021360954.
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| 245 |
1 |
0 |
|a Computational space flight mechanics
|h [electronic resource] /
|c Claus Weiland.
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| 260 |
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|a Berlin ;
|a Heidelberg :
|b Springer-Verlag,
|c ©2010.
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| 300 |
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|a 1 online resource (xiii, 300 pages)
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| 336 |
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|a text
|b txt
|2 rdacontent.
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| 337 |
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|a computer
|b c
|2 rdamedia.
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| 338 |
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|a online resource
|b cr
|2 rdacarrier.
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| 504 |
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|a Includes bibliographical references and indexes.
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|a Cover13; -- Title Page -- Preface -- Acknowledgements -- Table of Contents -- Chapter 1 Introduction -- References -- Chapter 2 Coordinate Transformations -- Basic Rotational Transformations -- Time Derivative of Vectors in Moving Frames -- The Velocity Vector -- The Acceleration Vector -- The Angular Velocity in a Body Frame: Euler Angles -- Problems -- References -- Chapter 3 Transformations between Often Used Coordinate Systems -- Transformation from Geodetic to Body Frame -- Transformation from Air Path to Body Frame -- Transformation from Geodetic to Flight Path Frame -- Transformation from Planetocentric to Orbital Frame -- Problems -- References -- Chapter 4 Kepler8217;s Laws of Planetary Motion and Newton8217;s Celestial Mechanics -- Kepler8217;s 1. Law -- Kepler8217;s 2. Law -- Kepler8217;s 3. Law -- Newton8217;s Celestial Mechanics -- Problems -- References -- Chapter 5 The Two-Body Problem -- The Equation of Motion -- The Energy Conservation -- The Angular Momentum Conservation -- The Orbit Equation -- The Various Orbits -- The Eccentricity e <1 -- The Eccentricity e 8805; 1 -- Test Cases for the Three Classes of Orbits -- Time Dependency of the Orbital Variables r and 952; and Kepler8217;s Equation -- The Elliptical Orbit -- Solutions of the Elliptical Test Case 1 -- The Hyperbolic Orbit -- Solutions of the Hyperbolic Test Case 3 -- The Classical Orbital Elements -- Derivation of Relations -- Sample Calculations of Test Case 1 Using Orbital Elements -- Sample Calculations of Test Case 1 Using the General Equations of Planetary Flight -- Perturbations of Orbital Dynamics -- Lagrange8217;s Planet Equations -- Numerical Solutions of Lagrange8217;s Planet Equations -- Numerical Solution of the General Equations of Planetary Flight for an Aspherical Earth -- Problems -- References -- Chapter 6 General Equations for Planetary Flight -- Equations of Translational Motion -- Flight without Bank Angle -- Flight with Bank Angle -- Equations Including Side Forces -- Flight with Propulsion Force -- Orbital Flight Around an Aspherical Earth -- Equations of Rotational Motion -- Set of Equations for Six Degree of Freedom Simulations -- Problems -- References -- Chapter 7 A Resum'{e} of the Aerothermodynamics of Space Flight Vehicles -- Conventions for Aerothermodynamic Data -- Flow Regimes and Physical Phenomena -- Aerothermodynamic Data of the X-38 Vehicle -- Data of Longitudinal Motion -- Data of Lateral Motion -- Problems -- References -- Chapter 8 Three and Six Degree of Freedom Trajectory Simulations -- Three Degree of Freedom Simulation for a Winged Space Vehicle -- Three Degree of Freedom Simulation for a Non-Winged Space Vehicle -- Six Degree of Freedom Simulations for a Winged Space Vehicle -- Flight with Statically Stable Longitudinal Motion -- Flight with Statically Stable Longitudinal and Yaw Motion -- Problems -- References -- Chapter 9 Numerical Applications of the General Equations for Planetary Flight -- Flight in Geostationary Orbit -- Flight in Low Earth Orbit -- Circular Equatorial Orbit (Inclination Angle 966; = 0) -- Circular Orbit with Inclination Angle 966; 3;= 0 -- Elliptical Orbits -- Elliptical Orbit without Aerodynamic Forces -- Elliptical Orbit with Aerodynamic Forces -- T$29.
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| 588 |
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|a Print version record.
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| 650 |
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|a Orbital mechanics.
|0 http://id.loc.gov/authorities/subjects/sh93000313.
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| 650 |
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|a Space flight.
|0 http://id.loc.gov/authorities/subjects/sh85125923.
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| 650 |
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|a Celestial mechanics.
|0 http://id.loc.gov/authorities/subjects/sh85082770.
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| 650 |
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7 |
|a Celestial mechanics.
|2 fast
|0 (OCoLC)fst00850133.
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| 650 |
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7 |
|a Orbital mechanics.
|2 fast
|0 (OCoLC)fst01047238.
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| 650 |
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7 |
|a Space flight.
|2 fast
|0 (OCoLC)fst01127676.
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| 776 |
0 |
8 |
|i Print version:
|a Weiland, Claus.
|t Computational space flight mechanics.
|d Berlin : Springer, ©2010
|z 9783642135828
|w (DLC) 2010930975
|w (OCoLC)646113728.
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| 856 |
4 |
0 |
|u https://colorado.idm.oclc.org/login?url=http://link.springer.com/10.1007/978-3-642-13583-5
|z Full Text (via Springer)
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|n 1
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