Orbital and Celestial Mechanics

Size: px
Start display at page:

Download "Orbital and Celestial Mechanics"

Transcription

1 Orbital and Celestial Mechanics John P. Vinti Edited by Gim J. Der TRW Los Angeles, California Nino L. Bonavito NASA Goddard Space Flight Center Greenbelt, Maryland Volume 177 PROGRESS IN ASTRONAUTICS AND AERONAUTICS Paul Zarchan, Editor-in-Chief Charles Stark Draper Laboratory, Inc. Cambridge, Massachusetts Published by the American Institute of Aeronautics and Astronautics, Inc Alexander Bell Drive, Reston, Virginia

2 Table of Contents Preface xv Introduction 1 Chapter 1 Newton's Laws 7 I. Newton's Laws of Motion 7 II. Newton's Law of Gravitation 7 III. The Gravitational Potential 8 IV. Gravitational Flux and Gauss' Theorem 10 V. Gravitational Properties of a True Sphere 11 Chapter 2 The Two-Body Problem 13 I. Reduction to the One-Center Problem 13 II. The One-Center Problem 14 III. The Laplace Vector 15 IV. The Conic Section Solutions 17 V. Elliptic Orbits 19 VI. Spherical Trigonometry 24 VII. Orbit in Space 24 VIII. Orbit Determination from Initial Values 29 Chapter 3 Lagrangian Dynamics ".". 31 I. Variations 31 II. D'Alembert's Principle 32 III. Hamilton's Principle : 32 IV. Lagrange's Equations \ 34 Reference 35 Chapter 4 The Hamiltonian Equations 37 I. An Important Theorem 39 II. Ignorable Variables 39 Chapter 5 Canonical Transformations 41 I. The Condition of Exact Differentials 41 II. Canonical Generating Functions 44 III. Extended Point Transformation 47 IV. Transformation from Plane Rectangular to Plane Polar Coordinates 47 V. The Jacobi Integral 49 References 51 Chapter 6 Hamilton-Jacobi Theory 53 I. The Hamilton-Jacobi Equation 53 ix

3 II. An Important Special Case 54 III. The Hamilton-Jacobi Equation for the Kepler Problem 55 IV. The Integrals for the Kepler Problem 58 V. Relations Connecting ^2 and /S3 with w and Q, 61 VI. Summary 69 Bibliography 70 Chapter 7 Hamilton-Jacobi Perturbation Theory 71 Bibliography 74 Chapter 8 The Vinti Spheroidal Method for Satellite Orbits and Ballistic Trajectories 75 I. Introduction 75 II. The Coordinates and the Hamiltonian 75 III. The Hamilton-Jacobi Equation 77 IV. Laplace's Equation 78 V. Expansion of Potential in Spherical Harmonics 79 VI. Return to the HJ Equation 81 VII. The Kinematic Equations 82 VIII. Orbital Elements 83 IX. Factoring the Quartics 84 X. The p Integrals 85 XI. The r] Integrals 90 XII. The Mean Frequencies 96 XIII. Assembly of the Kinematic Equations 99 XIV. Solution of the Kinematic Equations 99 XV. The Periodic Terms 101 XVI. The Right Ascension (p 102 XVII. Further Developments 103 References 105 Chapter 9 Delaunay Variables.\ 107 % Reference 108 Chapter 10 The Lagrange Planetary Equations 109 I. Semi-Major Axis 110 II. Eccentricity 110 III. Inclination 110 IV. Mean Anomaly :... Ill V. The Argument of Pericenter. 112 VI. The Longitude of the Node 112 VII. Summary 113 Reference 114 Chapter 11 The Planetary Disturbing Function 115 Bibliography. 117 Chapter 12 Gaussian Variational Equations for the Jacobi Elements 119 References 125

4 XI Chapter 13 Gaussian Variational Equations for the Keplerian Elements I. Preliminaries 127 II. Equations for dj and a 130 III. Equations for a.2 and e 132 IV. Equations for a 3 and / 133 V. Equations for $ 3 = & 135 VI. Equations for fi 2 = d> 136 VII. Equations for ft and I 140 VIII. Summary 144 Chapter 14 Potential Theory 145 I. Introduction 145 II. Laplace's Equation 147 III. The Eigenvalue Problem 151 IV. The R(r) Equation 153 V. The Assembled Solution 153 VI. Legendre Polynomials 154 VII. The Results for P n (x) 154 VIII. The Solution for m > References 156 Chapter 15 The Gravitational Potential of a Planet 157 I. The Addition Theorem for Spherical Harmonics 157 II. The Standard Series 161 III. Orthogonality of Spherical Harmonics 166 IV. The Normalized Coefficients and Harmonics 168 V. The Figure of the Earth 169 VI. Geoid as an Oblate Spheroid 172 References Chapter 16 " Elementary Theory of Satellite Orbits with Use of the Mean Anomaly 175 I. A Few Numbers \ 175 II. The Disturbing Function 175 III. Elliptic Expansions 177 IV. Solution of the Lagrange Variational Equations 184 V. Motion of Perigee, First Approximation 184 VI. Motion of the Node, First Approximation 186 VII. The Semi-Major Axis 187 VIII. The Inclination. 187 IX. The Eccentricity 188 X. Variation of the Mean Motion 189 XI. Variation of the Mean Anomaly 189 References 191 Chapter 17 Elementary Theory of Satellite Orbits with Use of the True Anomaly 193 I. Introduction 193 II. Derivatives with Respect to e 195 III. The Semi-Major Axis a 195

5 XII IV. The Eccentricity e 196 V. The Inclination / 197 VI. The Motion of the Node 198 VII. The Motion of Perigee 199 VIII. Variation of the Mean Anomaly 204 Reference 206 Chapter 18 The Effects of Drag on Satellite Orbits 207 I. Introduction 207 II. Components of the Drag in Terms of the Anomalies E and/ 209 III. Equations for a and e in Terms of the True Anomaly 210 IV. Secular Behavior of a, e, ft), and 211 V. Equations for a and e in Terms of the Eccentric Anomaly 212 VI. An Equation for 212 VII. Equations for the Integration 213 References 218 Chapter 19 The Brouwer-von Zeipel Method I 219 I. Introduction 219 II. Splitting F\ into Two Parts 220 HI. Elimination of I 220 IV. Short Periodic Terms of Order J V. Second-Order Terms, General 230 VI. A Second Canonical Transformation 232 VII. Results to This Point 235 VIII. Secular Terms 236 IX. Algorithm 239 References 240 Chapter 20 The Brouwer-von Zeipel Method II 241 I. Introduction 241 II. The Effects of / III. The Effects of 7 4 > 246 IV. The Average A 4 F 247 Reference 251 Chapter 21 Lagrange and Poisson Brackets 253 I. Introduction 253 II. Lagrange Brackets 254 III. The Jacobi Relations 255 IV. Poisson Brackets 257 V. Invariance of a Poisson Bracket to a Contact Transformation 258 VI. Other Relations for Poisson Brackets 259 References 262 Chapter 22 Lie Series 263 I. Introduction 263 II. Hori's Section III. Theorems 263 References 273

6 XIII Chapter 23 Perturbations by Lie Series 275 I. Introduction 275 II. Lie Transformations 275 III. Application to Satellite Orbits 277 IV. Elimination of the Mean Anomaly 278 V. Comparison with Brouwer's Theory 280 VI. A Second Lie Transformation 285 References 289 Chapter 24 The General Three-Body Problem 291 I. Introduction 291 II. Formulation of the General Three-Body Problem 291 III. Momentum Integrals 291 IV. Angular Momentum 292 V. Energy 293 VI. Stationary Solutions 294 VII. The Triangular Stationary Solution 295 VIII. The Collinear Stationary Solution. 296 Reference 298 Chapter 25 The Restricted Three-Body Problem 299 I. Introduction 299 II. Zero-Velocity Curves 304 III. Equilibrium Points 305 IV. Motion near the Equilibrium Points 312 V. Motion in the Plane of the Primaries 313 VI. Further Considerations About L 4 and L$ 320 VII. Further Considerations About the Collinear Points 323 References 327 Chapter 26 Staeckel Systems 329 I. Staeckel's Theorem 329 II. Staeckel Systems 332 III. The Staeckel Integrals \ 333 IV. An Example: The Kepler Problem 334 V. General Remarks About Separable Systems 335 VI. Motion According to*2 = F(x) 335 VII. Conditionally Periodic Staeckel Systems 337 VIII. Action and Angle Variables 341 IX. Keplerian Action Variables X. Conditionally Periodic Staeckel Systems, Continued 347 References 352 Appendix A Coordinate Systems and Coordinate Transformations 353 I. Coordinate Systems 353 II. Coordinate Transformations 364 References 365 Appendix B Vinti Spheroidal Method Computational Procedure and Trajectory Propagators 367 I. The Kepler Problem 368 II. Given Constants 368

7 XIV III. The vinti3 Computation Procedure 369 IV. The vinti6 Computation Procedure 371 V. Summary of the Vinti Trajectory Propagators 374 References Appendix C Examples 377 I. Low-Earth Orbit 378 II. High-Earth Orbit 379 III. Molniya Orbit 379 IV. Geosynchronous Orbit 380 V. Parabolic Orbit of 0 Inclination 381 VI. "Parabolic Orbit" of 0 Inclination in the Oblate Spheroidal System VII. Hyperbolic Orbit of 0 Inclination 382 VIII. Hyperbolic Orbit of 90 Inclination 383 IX. Long-Range Ballistic Missile Trajectory 384 X. Exo-Atmospheric Interceptor Trajectory 384 Appendix D How to Use the Vinti Routines 387 I. The Source Folder 387 II. The Examples Folder 387 III. The Users 388 IV. Some Editing Problems 389 Appendix E Bibliography 391 I. Papers Published by the Author 391 II. Papers Acknowledging Vinti's Work 394 III. Books Acknowledging Vinti's Work 396 Index 397

Analytical Mechanics. of Space Systems. tfa AA. Hanspeter Schaub. College Station, Texas. University of Colorado Boulder, Colorado.

Analytical Mechanics. of Space Systems. tfa AA. Hanspeter Schaub. College Station, Texas. University of Colorado Boulder, Colorado. Analytical Mechanics of Space Systems Third Edition Hanspeter Schaub University of Colorado Boulder, Colorado John L. Junkins Texas A&M University College Station, Texas AIM EDUCATION SERIES Joseph A.

More information

Ulrich Walter. Astronautics. The Physics of Space Flight. 2nd, Enlarged and Improved Edition

Ulrich Walter. Astronautics. The Physics of Space Flight. 2nd, Enlarged and Improved Edition Ulrich Walter Astronautics The Physics of Space Flight 2nd, Enlarged and Improved Edition Preface to Second Edition Preface XVII Acknowledgments XIX List of Symbols XXI XV 1 Rocket Fundamentals 1 1.1 Rocket

More information

Fundamentals of Astrodynamics and Applications

Fundamentals of Astrodynamics and Applications Fundamentals of Astrodynamics and Applications Third Edition David A. Vallado with technical contributions by Wayne D. McClain Space Technology Library Published Jointly by Microcosm Press Hawthorne, CA

More information

An Introduction to Celestial Mechanics

An Introduction to Celestial Mechanics An Introduction to Celestial Mechanics This accessible text on classical celestial mechanics the principles governing the motions of bodies in the solar system provides a clear and concise treatment of

More information

CELESTIAL MECHANICS. Part I. Mathematical Preambles

CELESTIAL MECHANICS. Part I. Mathematical Preambles Chapter 1. Numerical Methods CELESTIAL MECHANICS Part I. Mathematical Preambles 1.1 Introduction 1.2 Numerical Integration 1.3 Quadratic Equations 1.4 The Solution of f(x) = 0 1.5 The Solution of Polynomial

More information

THE THREE-BODY PROBLEM

THE THREE-BODY PROBLEM STUDIES IN ASTRONAUTICS 4 THE THREE-BODY PROBLEM CHRISTIAN MARCH AL Office National d'etudes et de RecherchesAerospatiales, Chätillon, France Amsterdam - Oxford - New York -Tokyo 1990 X CONTENTS Foreword

More information

THIRD-BODY PERTURBATION USING A SINGLE AVERAGED MODEL

THIRD-BODY PERTURBATION USING A SINGLE AVERAGED MODEL INPE-1183-PRE/67 THIRD-BODY PERTURBATION USING A SINGLE AVERAGED MODEL Carlos Renato Huaura Solórzano Antonio Fernando Bertachini de Almeida Prado ADVANCES IN SPACE DYNAMICS : CELESTIAL MECHANICS AND ASTRONAUTICS,

More information

METHODS OF THEORETICAL PHYSICS

METHODS OF THEORETICAL PHYSICS METHODS OF THEORETICAL PHYSICS Philip M. Morse PROFESSOR OF PHYSICS MASSACHUSETTS INSTITUTE OF TECHNOLOGY Herman Feshbach PROFESSOR OF PHYSICS MASSACHUSETTS INSTITUTE OF TECHNOLOGY PART II: CHAPTERS 9

More information

Boundary. DIFFERENTIAL EQUATIONS with Fourier Series and. Value Problems APPLIED PARTIAL. Fifth Edition. Richard Haberman PEARSON

Boundary. DIFFERENTIAL EQUATIONS with Fourier Series and. Value Problems APPLIED PARTIAL. Fifth Edition. Richard Haberman PEARSON APPLIED PARTIAL DIFFERENTIAL EQUATIONS with Fourier Series and Boundary Value Problems Fifth Edition Richard Haberman Southern Methodist University PEARSON Boston Columbus Indianapolis New York San Francisco

More information

Satellite Communications

Satellite Communications Satellite Communications Lecture (3) Chapter 2.1 1 Gravitational Force Newton s 2nd Law: r r F = m a Newton s Law Of Universal Gravitation (assuming point masses or spheres): Putting these together: r

More information

APPLIED PARTIM DIFFERENTIAL EQUATIONS with Fourier Series and Boundary Value Problems

APPLIED PARTIM DIFFERENTIAL EQUATIONS with Fourier Series and Boundary Value Problems APPLIED PARTIM DIFFERENTIAL EQUATIONS with Fourier Series and Boundary Value Problems Fourth Edition Richard Haberman Department of Mathematics Southern Methodist University PEARSON Prentice Hall PEARSON

More information

PRINCIPLES OF PHYSICS. \Hp. Ni Jun TSINGHUA. Physics. From Quantum Field Theory. to Classical Mechanics. World Scientific. Vol.2. Report and Review in

PRINCIPLES OF PHYSICS. \Hp. Ni Jun TSINGHUA. Physics. From Quantum Field Theory. to Classical Mechanics. World Scientific. Vol.2. Report and Review in LONDON BEIJING HONG TSINGHUA Report and Review in Physics Vol2 PRINCIPLES OF PHYSICS From Quantum Field Theory to Classical Mechanics Ni Jun Tsinghua University, China NEW JERSEY \Hp SINGAPORE World Scientific

More information

Analytical Mechanics for Relativity and Quantum Mechanics

Analytical Mechanics for Relativity and Quantum Mechanics Analytical Mechanics for Relativity and Quantum Mechanics Oliver Davis Johns San Francisco State University OXPORD UNIVERSITY PRESS CONTENTS Dedication Preface Acknowledgments v vii ix PART I INTRODUCTION:

More information

The Superior Lambert Algorithm

The Superior Lambert Algorithm The Superior Lambert Algorithm Gim J. Der DerAstrodynamics Abstract Lambert algorithms are used extensively for initial orbit determination, mission planning, space debris correlation, and missile targeting,

More information

5.12 The Aerodynamic Assist Trajectories of Vehicles Propelled by Solar Radiation Pressure References...

5.12 The Aerodynamic Assist Trajectories of Vehicles Propelled by Solar Radiation Pressure References... 1 The Two-Body Problem... 1 1.1 Position of the Problem... 1 1.2 The Conic Sections and Their Geometrical Properties... 12 1.3 The Elliptic Orbits... 20 1.4 The Hyperbolic and Parabolic Trajectories...

More information

Celestial Mechanics and Satellite Orbits

Celestial Mechanics and Satellite Orbits Celestial Mechanics and Satellite Orbits Introduction to Space 2017 Slides: Jaan Praks, Hannu Koskinen, Zainab Saleem Lecture: Jaan Praks Assignment Draw Earth, and a satellite orbiting the Earth. Draw

More information

ANALYTICAL MECHANICS. LOUIS N. HAND and JANET D. FINCH CAMBRIDGE UNIVERSITY PRESS

ANALYTICAL MECHANICS. LOUIS N. HAND and JANET D. FINCH CAMBRIDGE UNIVERSITY PRESS ANALYTICAL MECHANICS LOUIS N. HAND and JANET D. FINCH CAMBRIDGE UNIVERSITY PRESS Preface xi 1 LAGRANGIAN MECHANICS l 1.1 Example and Review of Newton's Mechanics: A Block Sliding on an Inclined Plane 1

More information

Introduction to Applied Nonlinear Dynamical Systems and Chaos

Introduction to Applied Nonlinear Dynamical Systems and Chaos Stephen Wiggins Introduction to Applied Nonlinear Dynamical Systems and Chaos Second Edition With 250 Figures 4jj Springer I Series Preface v L I Preface to the Second Edition vii Introduction 1 1 Equilibrium

More information

Theorem of the keplerian kinematics

Theorem of the keplerian kinematics 1 Theorem of the keplerian kinematics Hervé Le Cornec, France, herve.le.cornec@free.fr Abstract : Any mobile having a velocity which is the addition of a rotation velocity and a translation velocity, both

More information

Modern Geometric Structures and Fields

Modern Geometric Structures and Fields Modern Geometric Structures and Fields S. P. Novikov I.A.TaJmanov Translated by Dmitry Chibisov Graduate Studies in Mathematics Volume 71 American Mathematical Society Providence, Rhode Island Preface

More information

CELESTIAL MECHANICS. Celestial Mechanics No. of Pages: 520 ISBN: (ebook) ISBN: (Print Volume)

CELESTIAL MECHANICS. Celestial Mechanics No. of Pages: 520 ISBN: (ebook) ISBN: (Print Volume) CELESTIAL MECHANICS Celestial Mechanics No. of Pages: 520 ISBN: 978-1-78021-019-3 (ebook) ISBN: 978-1-78021-519-8 (Print Volume) For more information of e-book and Print Volume(s) order, please click here

More information

Introduction to Aircraft Flight. Mechanics

Introduction to Aircraft Flight. Mechanics Introduction to Aircraft Flight. Mechanics i Performance, Static Stability, Dynamic Stability, Classical Feedback Control, and State-Space Foundations Second Edition Thomas R. Yechout with contributions

More information

2.5.1 Static tides Tidal dissipation Dynamical tides Bibliographical notes Exercises 118

2.5.1 Static tides Tidal dissipation Dynamical tides Bibliographical notes Exercises 118 ii Contents Preface xiii 1 Foundations of Newtonian gravity 1 1.1 Newtonian gravity 2 1.2 Equations of Newtonian gravity 3 1.3 Newtonian field equation 7 1.4 Equations of hydrodynamics 9 1.4.1 Motion of

More information

Contents. 1 Basic Equations 1. Acknowledgment. 1.1 The Maxwell Equations Constitutive Relations 11

Contents. 1 Basic Equations 1. Acknowledgment. 1.1 The Maxwell Equations Constitutive Relations 11 Preface Foreword Acknowledgment xvi xviii xix 1 Basic Equations 1 1.1 The Maxwell Equations 1 1.1.1 Boundary Conditions at Interfaces 4 1.1.2 Energy Conservation and Poynting s Theorem 9 1.2 Constitutive

More information

FINAL EXAM GROUND RULES

FINAL EXAM GROUND RULES PHYSICS 507 Fall 2011 FINAL EXAM Room: ARC-108 Time: Wednesday, December 21, 10am-1pm GROUND RULES There are four problems based on the above-listed material. Closed book Closed notes Partial credit will

More information

List of Tables. Table 3.1 Determination efficiency for circular orbits - Sample problem 1 41

List of Tables. Table 3.1 Determination efficiency for circular orbits - Sample problem 1 41 List of Tables Table 3.1 Determination efficiency for circular orbits - Sample problem 1 41 Table 3.2 Determination efficiency for elliptical orbits Sample problem 2 42 Table 3.3 Determination efficiency

More information

Analysis of frozen orbits for solar sails

Analysis of frozen orbits for solar sails Trabalho apresentado no XXXV CNMAC, Natal-RN, 2014. Analysis of frozen orbits for solar sails J. P. S. Carvalho, R. Vilhena de Moraes, Instituto de Ciência e Tecnologia, UNIFESP, São José dos Campos -

More information

Quantum Mechanics: Foundations and Applications

Quantum Mechanics: Foundations and Applications Arno Böhm Quantum Mechanics: Foundations and Applications Third Edition, Revised and Enlarged Prepared with Mark Loewe With 96 Illustrations Springer-Verlag New York Berlin Heidelberg London Paris Tokyo

More information

Preface. 2 Linear Equations and Eigenvalue Problem 22

Preface. 2 Linear Equations and Eigenvalue Problem 22 Contents Preface xv 1 Errors in Computation 1 1.1 Introduction 1 1.2 Floating Point Representation of Number 1 1.3 Binary Numbers 2 1.3.1 Binary number representation in computer 3 1.4 Significant Digits

More information

ANNEX 1. DEFINITION OF ORBITAL PARAMETERS AND IMPORTANT CONCEPTS OF CELESTIAL MECHANICS

ANNEX 1. DEFINITION OF ORBITAL PARAMETERS AND IMPORTANT CONCEPTS OF CELESTIAL MECHANICS ANNEX 1. DEFINITION OF ORBITAL PARAMETERS AND IMPORTANT CONCEPTS OF CELESTIAL MECHANICS A1.1. Kepler s laws Johannes Kepler (1571-1630) discovered the laws of orbital motion, now called Kepler's laws.

More information

OPTIMAL SPACECRAF1 ROTATIONAL MANEUVERS

OPTIMAL SPACECRAF1 ROTATIONAL MANEUVERS STUDIES IN ASTRONAUTICS 3 OPTIMAL SPACECRAF1 ROTATIONAL MANEUVERS JOHNL.JUNKINS Texas A&M University, College Station, Texas, U.S.A. and JAMES D.TURNER Cambridge Research, Division of PRA, Inc., Cambridge,

More information

THE exploration of planetary satellites is currently an active area

THE exploration of planetary satellites is currently an active area JOURNAL OF GUIDANCE, CONTROL, AND DYNAMICS Vol. 9, No. 5, September October 6 Design of Science Orbits About Planetary Satellites: Application to Europa Marci E. Paskowitz and Daniel J. Scheeres University

More information

APPLIED PARTIAL DIFFERENTIAL EQUATIONS

APPLIED PARTIAL DIFFERENTIAL EQUATIONS APPLIED PARTIAL DIFFERENTIAL EQUATIONS AN I N T R O D U C T I O N ALAN JEFFREY University of Newcastle-upon-Tyne ACADEMIC PRESS An imprint of Elsevier Science Amsterdam Boston London New York Oxford Paris

More information

Section 13. Orbit Perturbation. Orbit Perturbation. Atmospheric Drag. Orbit Lifetime

Section 13. Orbit Perturbation. Orbit Perturbation. Atmospheric Drag. Orbit Lifetime Section 13 Orbit Perturbation Orbit Perturbation A satellite s orbit around the Earth is affected by o Asphericity of the Earth s gravitational potential : Most significant o Atmospheric drag : Orbital

More information

Long-Term Evolution of High Earth Orbits: Effects of Direct Solar Radiation Pressure and Comparison of Trajectory Propagators

Long-Term Evolution of High Earth Orbits: Effects of Direct Solar Radiation Pressure and Comparison of Trajectory Propagators Long-Term Evolution of High Earth Orbits: Effects of Direct Solar Radiation Pressure and Comparison of Trajectory Propagators by L. Anselmo and C. Pardini (Luciano.Anselmo@isti.cnr.it & Carmen.Pardini@isti.cnr.it)

More information

Chapter 2: Orbits and Launching Methods

Chapter 2: Orbits and Launching Methods 9/20/ Chapter 2: Orbits and Launching Methods Prepared by Dr. Mohammed Taha El Astal EELE 6335 Telecom. System Part I: Satellite Communic ations Winter Content Kepler s First, Second, and Third Law Definitions

More information

ADVANCED ENGINEERING MATHEMATICS

ADVANCED ENGINEERING MATHEMATICS ADVANCED ENGINEERING MATHEMATICS DENNIS G. ZILL Loyola Marymount University MICHAEL R. CULLEN Loyola Marymount University PWS-KENT O I^7 3 PUBLISHING COMPANY E 9 U Boston CONTENTS Preface xiii Parti ORDINARY

More information

Introduction. Finite and Spectral Element Methods Using MATLAB. Second Edition. C. Pozrikidis. University of Massachusetts Amherst, USA

Introduction. Finite and Spectral Element Methods Using MATLAB. Second Edition. C. Pozrikidis. University of Massachusetts Amherst, USA Introduction to Finite and Spectral Element Methods Using MATLAB Second Edition C. Pozrikidis University of Massachusetts Amherst, USA (g) CRC Press Taylor & Francis Group Boca Raton London New York CRC

More information

Gossamer Spacecraft: Membrane and Inflatable Structures Technology for Space Applications

Gossamer Spacecraft: Membrane and Inflatable Structures Technology for Space Applications Gossamer Spacecraft: Membrane and Inflatable Structures Technology for Space Applications Edited by Christopher H. M. Jenkins South Dakota School of Mines Volume 191 PROGRESS IN ASTRONAUTICS AND AERONAUTICS

More information

THE MECHANICAL UNIVERSE

THE MECHANICAL UNIVERSE THE MECHANICAL UNIVERSE MECHANICS AND HEAT, ADVANCED EDITION STEVEN С FRAUTSCHI PROFESSOR OF THEORETICAL PHYSICS CALIFORNIA INSTITUTE OF TECHNOLOGY RICHARD P. OLENICK ASSISTANT PROFESSOR OF PHYSICS, UNIVERSITY

More information

Adaptive Filtering. Squares. Alexander D. Poularikas. Fundamentals of. Least Mean. with MATLABR. University of Alabama, Huntsville, AL.

Adaptive Filtering. Squares. Alexander D. Poularikas. Fundamentals of. Least Mean. with MATLABR. University of Alabama, Huntsville, AL. Adaptive Filtering Fundamentals of Least Mean Squares with MATLABR Alexander D. Poularikas University of Alabama, Huntsville, AL CRC Press Taylor & Francis Croup Boca Raton London New York CRC Press is

More information

Previous Lecture. Orbital maneuvers: general framework. Single-impulse maneuver: compatibility conditions

Previous Lecture. Orbital maneuvers: general framework. Single-impulse maneuver: compatibility conditions 2 / 48 Previous Lecture Orbital maneuvers: general framework Single-impulse maneuver: compatibility conditions closed form expression for the impulsive velocity vector magnitude interpretation coplanar

More information

Contents. I Basic Methods 13

Contents. I Basic Methods 13 Preface xiii 1 Introduction 1 I Basic Methods 13 2 Convergent and Divergent Series 15 2.1 Introduction... 15 2.1.1 Power series: First steps... 15 2.1.2 Further practical aspects... 17 2.2 Differential

More information

Previous Lecture. The Von Zeipel Method. Application 1: The Brouwer model. Application 2: The Cid-Lahulla model. Simplified Brouwer transformation.

Previous Lecture. The Von Zeipel Method. Application 1: The Brouwer model. Application 2: The Cid-Lahulla model. Simplified Brouwer transformation. 2 / 36 Previous Lecture The Von Zeipel Method. Application 1: The Brouwer model. Application 2: The Cid-Lahulla model. Simplified Brouwer transformation. Review of Analytic Models 3 / 36 4 / 36 Review:

More information

Static & Dynamic. Analysis of Structures. Edward L.Wilson. University of California, Berkeley. Fourth Edition. Professor Emeritus of Civil Engineering

Static & Dynamic. Analysis of Structures. Edward L.Wilson. University of California, Berkeley. Fourth Edition. Professor Emeritus of Civil Engineering Static & Dynamic Analysis of Structures A Physical Approach With Emphasis on Earthquake Engineering Edward LWilson Professor Emeritus of Civil Engineering University of California, Berkeley Fourth Edition

More information

Fluid Dynamics: Theory, Computation, and Numerical Simulation Second Edition

Fluid Dynamics: Theory, Computation, and Numerical Simulation Second Edition Fluid Dynamics: Theory, Computation, and Numerical Simulation Second Edition C. Pozrikidis m Springer Contents Preface v 1 Introduction to Kinematics 1 1.1 Fluids and solids 1 1.2 Fluid parcels and flow

More information

The Fractional Fourier Transform with Applications in Optics and Signal Processing

The Fractional Fourier Transform with Applications in Optics and Signal Processing * The Fractional Fourier Transform with Applications in Optics and Signal Processing Haldun M. Ozaktas Bilkent University, Ankara, Turkey Zeev Zalevsky Tel Aviv University, Tel Aviv, Israel M. Alper Kutay

More information

Gravitation. Kepler s Law. BSc I SEM II (UNIT I)

Gravitation. Kepler s Law. BSc I SEM II (UNIT I) Gravitation Kepler s Law BSc I SEM II (UNIT I) P a g e 2 Contents 1) Newton s Law of Gravitation 3 Vector representation of Newton s Law of Gravitation 3 Characteristics of Newton s Law of Gravitation

More information

Tyn Myint-U Lokenath Debnath. Linear Partial Differential Equations for Scientists and Engineers. Fourth Edition. Birkhauser Boston Basel Berlin

Tyn Myint-U Lokenath Debnath. Linear Partial Differential Equations for Scientists and Engineers. Fourth Edition. Birkhauser Boston Basel Berlin Tyn Myint-U Lokenath Debnath Linear Partial Differential Equations for Scientists and Engineers Fourth Edition Birkhauser Boston Basel Berlin Preface to the Fourth Edition Preface to the Third Edition

More information

Partial Differential Equations

Partial Differential Equations Partial Differential Equations Analytical Solution Techniques J. Kevorkian University of Washington Wadsworth & Brooks/Cole Advanced Books & Software Pacific Grove, California C H A P T E R 1 The Diffusion

More information

Extending the Patched-Conic Approximation to the Restricted Four-Body Problem

Extending the Patched-Conic Approximation to the Restricted Four-Body Problem Monografías de la Real Academia de Ciencias de Zaragoza 3, 133 146, (6). Extending the Patched-Conic Approximation to the Restricted Four-Body Problem Thomas R. Reppert Department of Aerospace and Ocean

More information

Cambridge University Press The Geometry of Celestial Mechanics: London Mathematical Society Student Texts 83 Hansjörg Geiges

Cambridge University Press The Geometry of Celestial Mechanics: London Mathematical Society Student Texts 83 Hansjörg Geiges acceleration, xii action functional, 173 and Newton s equation (Maupertuis s principle), 173 action of a group on a set, 206 transitive, 157 affine part of a subset of RP 2, 143 algebraic multiplicity

More information

A SEMI-ANALYTICAL ORBIT PROPAGATOR PROGRAM FOR HIGHLY ELLIPTICAL ORBITS

A SEMI-ANALYTICAL ORBIT PROPAGATOR PROGRAM FOR HIGHLY ELLIPTICAL ORBITS A SEMI-ANALYTICAL ORBIT PROPAGATOR PROGRAM FOR HIGHLY ELLIPTICAL ORBITS M. Lara, J. F. San Juan and D. Hautesserres Scientific Computing Group and Centre National d Études Spatiales 6th International Conference

More information

Parallel Algorithm for Track Initiation for Optical Space Surveillance

Parallel Algorithm for Track Initiation for Optical Space Surveillance Parallel Algorithm for Track Initiation for Optical Space Surveillance 3 rd US-China Technical Interchange on Space Surveillance Beijing Institute of Technology Beijing, China 12 16 May 2013 Dr. Paul W.

More information

Chapter 5 - Part 1. Orbit Perturbations. D.Mortari - AERO-423

Chapter 5 - Part 1. Orbit Perturbations. D.Mortari - AERO-423 Chapter 5 - Part 1 Orbit Perturbations D.Mortari - AERO-43 Orbital Elements Orbit normal i North Orbit plane Equatorial plane ϕ P O ω Ω i Vernal equinox Ascending node D. Mortari - AERO-43 Introduction

More information

Elementary Lie Group Analysis and Ordinary Differential Equations

Elementary Lie Group Analysis and Ordinary Differential Equations Elementary Lie Group Analysis and Ordinary Differential Equations Nail H. Ibragimov University of North-West Mmabatho, South Africa JOHN WILEY & SONS Chichester New York Weinheim Brisbane Singapore Toronto

More information

An Introduction to Probability Theory and Its Applications

An Introduction to Probability Theory and Its Applications An Introduction to Probability Theory and Its Applications WILLIAM FELLER (1906-1970) Eugene Higgins Professor of Mathematics Princeton University VOLUME II SECOND EDITION JOHN WILEY & SONS Contents I

More information

Analysis of Lunisolar Resonances. in an Artificial Satellite Orbits

Analysis of Lunisolar Resonances. in an Artificial Satellite Orbits Applied Mathematical Sciences, Vol., 008, no., 0 0 Analysis of Lunisolar Resonances in an Artificial Satellite Orbits F. A. Abd El-Salam, Yehia A. Abdel-Aziz,*, M. El-Saftawy, and M. Radwan Cairo university,

More information

REVIEW. Hamilton s principle. based on FW-18. Variational statement of mechanics: (for conservative forces) action Equivalent to Newton s laws!

REVIEW. Hamilton s principle. based on FW-18. Variational statement of mechanics: (for conservative forces) action Equivalent to Newton s laws! Hamilton s principle Variational statement of mechanics: (for conservative forces) action Equivalent to Newton s laws! based on FW-18 REVIEW the particle takes the path that minimizes the integrated difference

More information

CLASSICAL ELECTRICITY

CLASSICAL ELECTRICITY CLASSICAL ELECTRICITY AND MAGNETISM by WOLFGANG K. H. PANOFSKY Stanford University and MELBA PHILLIPS Washington University SECOND EDITION ADDISON-WESLEY PUBLISHING COMPANY Reading, Massachusetts Menlo

More information

B.Sc. (Semester - 5) Subject: Physics Course: US05CPHY01 Classical Mechanics

B.Sc. (Semester - 5) Subject: Physics Course: US05CPHY01 Classical Mechanics 1 B.Sc. (Semester - 5) Subject: Physics Course: US05CPHY01 Classical Mechanics Question Bank UNIT: I Multiple choice questions: (1) The gravitational force between two masses is (a) Repulsive (b) Attractive

More information

METHODS OF ENGINEERING MATHEMATICS

METHODS OF ENGINEERING MATHEMATICS METHODS OF ENGINEERING MATHEMATICS Edward J. Hang Kyung K. Choi Department of Mechanical Engineering College of Engineering The University of Iowa Iowa City, Iowa 52242 METHODS OF ENGINEERING MATHEMATICS

More information

Experimental Analysis of Low Earth Orbit Satellites due to Atmospheric Perturbations

Experimental Analysis of Low Earth Orbit Satellites due to Atmospheric Perturbations Experimental Analysis of Low Earth Orbit Satellites due to Atmospheric Perturbations Aman Saluja #1, Manish Bansal #2, M Raja #3, Mohd Maaz #4 #Aerospace Department, University of Petroleum and Energy

More information

AIR FORCE INSTITUTE OF TECHNOLOGY

AIR FORCE INSTITUTE OF TECHNOLOGY Effects of Air Drag and Lunar Third-Body Pertubrations on Orbital Motion Near a Reference KAM Torus THESIS Luke J. Hagen, Captain, USAF AFIT/GA/ENY/11-M06 DEPARTMENT OF THE AIR FORCE AIR UNIVERSITY AIR

More information

Satellite meteorology

Satellite meteorology GPHS 422 Satellite meteorology GPHS 422 Satellite meteorology Lecture 1 6 July 2012 Course outline 2012 2 Course outline 2012 - continued 10:00 to 12:00 3 Course outline 2012 - continued 4 Some reading

More information

ORBITAL DECAY PREDICTION AND SPACE DEBRIS IMPACT ON NANO-SATELLITES

ORBITAL DECAY PREDICTION AND SPACE DEBRIS IMPACT ON NANO-SATELLITES Journal of Science and Arts Year 16, No. 1(34), pp. 67-76, 2016 ORIGINAL PAPER ORBITAL DECAY PREDICTION AND SPACE DEBRIS IMPACT ON NANO-SATELLITES MOHAMMED CHESSAB MAHDI 1 Manuscript received: 22.02.2016;

More information

INTRODUCTION TO THE CALCULUS OF VARIATIONS AND ITS APPLICATIONS

INTRODUCTION TO THE CALCULUS OF VARIATIONS AND ITS APPLICATIONS INTRODUCTION TO THE CALCULUS OF VARIATIONS AND ITS APPLICATIONS Frederick Y.M. Wan University of California, Irvine CHAPMAN & HALL I(J)P An International Thomson Publishing Company New York Albany Bonn

More information

Study of the Fuel Consumption for Station-Keeping Maneuvers for GEO satellites based on the Integral of the Perturbing Forces over Time

Study of the Fuel Consumption for Station-Keeping Maneuvers for GEO satellites based on the Integral of the Perturbing Forces over Time Study of the Fuel Consumption for Station-Keeping Maneuvers for GEO satellites based on the Integral of the Perturbing Forces over Time THAIS CARNEIRO OLIVEIRA 1 ; ANTONIO FERNANDO BERTACHINI DE ALMEIDA

More information

Lessons in Estimation Theory for Signal Processing, Communications, and Control

Lessons in Estimation Theory for Signal Processing, Communications, and Control Lessons in Estimation Theory for Signal Processing, Communications, and Control Jerry M. Mendel Department of Electrical Engineering University of Southern California Los Angeles, California PRENTICE HALL

More information

Optimization of Orbital Transfer of Electrodynamic Tether Satellite by Nonlinear Programming

Optimization of Orbital Transfer of Electrodynamic Tether Satellite by Nonlinear Programming Optimization of Orbital Transfer of Electrodynamic Tether Satellite by Nonlinear Programming IEPC-2015-299 /ISTS-2015-b-299 Presented at Joint Conference of 30th International Symposium on Space Technology

More information

Numerical Methods for Engineers and Scientists

Numerical Methods for Engineers and Scientists Numerical Methods for Engineers and Scientists Second Edition Revised and Expanded Joe D. Hoffman Department of Mechanical Engineering Purdue University West Lafayette, Indiana m MARCEL D E К К E R MARCEL

More information

ELEMENTARY MATRIX ALGEBRA

ELEMENTARY MATRIX ALGEBRA ELEMENTARY MATRIX ALGEBRA Third Edition FRANZ E. HOHN DOVER PUBLICATIONS, INC. Mineola, New York CONTENTS CHAPTER \ Introduction to Matrix Algebra 1.1 Matrices 1 1.2 Equality of Matrices 2 13 Addition

More information

Topics for the Qualifying Examination

Topics for the Qualifying Examination Topics for the Qualifying Examination Quantum Mechanics I and II 1. Quantum kinematics and dynamics 1.1 Postulates of Quantum Mechanics. 1.2 Configuration space vs. Hilbert space, wave function vs. state

More information

SATELLITE RELATIVE MOTION PROPAGATION AND CONTROL. A Thesis PRASENJIT SENGUPTA

SATELLITE RELATIVE MOTION PROPAGATION AND CONTROL. A Thesis PRASENJIT SENGUPTA SATELLITE RELATIVE MOTION PROPAGATION AND CONTROL IN THE PRESENCE OF J 2 PERTURBATIONS A Thesis by PRASENJIT SENGUPTA Submitted to the Office of Graduate Studies of Texas A&M University in partial fulfillment

More information

Lunisolar Secular Resonances

Lunisolar Secular Resonances Lunisolar Secular Resonances Jessica Pillow Supervisor: Dr. Aaron J. Rosengren December 15, 2017 1 Introduction The study of the dynamics of objects in Earth s orbit has recently become very popular in

More information

Theorem of the Keplerian kinematics

Theorem of the Keplerian kinematics myjournal manuscript No. (will be inserted by the editor) Theorem of the Keplerian kinematics Herve Le Cornec Received: date / Accepted: date Abstract As described in the literature the speed of a Keplerian

More information

Searching for less perturbed elliptical orbits around Europa

Searching for less perturbed elliptical orbits around Europa Journal of Physics: Conference Series PAPER OPEN ACCESS Searching for less perturbed elliptical orbits around Europa To cite this article: J Cardoso dos Santos et al 2015 J. Phys.: Conf. Ser. 641 012011

More information

Physical Dynamics (SPA5304) Lecture Plan 2018

Physical Dynamics (SPA5304) Lecture Plan 2018 Physical Dynamics (SPA5304) Lecture Plan 2018 The numbers on the left margin are approximate lecture numbers. Items in gray are not covered this year 1 Advanced Review of Newtonian Mechanics 1.1 One Particle

More information

The Transition to Chaos

The Transition to Chaos Linda E. Reichl The Transition to Chaos Conservative Classical Systems and Quantum Manifestations Second Edition With 180 Illustrations v I.,,-,,t,...,* ', Springer Dedication Acknowledgements v vii 1

More information

Shigeji Fujita and Salvador V Godoy. Mathematical Physics WILEY- VCH. WILEY-VCH Verlag GmbH & Co. KGaA

Shigeji Fujita and Salvador V Godoy. Mathematical Physics WILEY- VCH. WILEY-VCH Verlag GmbH & Co. KGaA Shigeji Fujita and Salvador V Godoy Mathematical Physics WILEY- VCH WILEY-VCH Verlag GmbH & Co. KGaA Contents Preface XIII Table of Contents and Categories XV Constants, Signs, Symbols, and General Remarks

More information

Federal Board HSSC-I Examination Physics Model Question Paper

Federal Board HSSC-I Examination Physics Model Question Paper Roll No: Signature of Candidate: Answer Sheet No: Signature of Invigilator: Federal Board HSSC-I Examination Physics Model Question Paper SECTION A Time allowed: 25 minutes Marks: 17 Note: Section-A is

More information

MISSION PERFORMANCE MEASURES FOR SPACECRAFT FORMATION FLYING

MISSION PERFORMANCE MEASURES FOR SPACECRAFT FORMATION FLYING MISSION PERFORMANCE MEASURES FOR SPACECRAFT FORMATION FLYING Steven P. Hughes and Christopher D. Hall Aerospace and Ocean Engineering Virginia Polytechnic Institute and State University ABSTRACT Clusters

More information

The precession of the perihelion of Mercury explained by Celestial Mechanics of Laplace Valdir Monteiro dos Santos Godoi

The precession of the perihelion of Mercury explained by Celestial Mechanics of Laplace Valdir Monteiro dos Santos Godoi The precession of the perihelion of Mercury explained by Celestial Mechanics of Laplace Valdir Monteiro dos Santos Godoi valdir.msgodoi@gmail.com ABSTRACT We calculate in this article an exact theoretical

More information

A SEARCH FOR INVARIANT RELATIVE SATELLITE MOTION

A SEARCH FOR INVARIANT RELATIVE SATELLITE MOTION A SEARCH FOR INVARIANT RELATIVE SATELLITE MOTION Marco Sabatini, Riccardo Bevilacqua, Mauro Pantaleoni, Dario Izzo * University of Roma La Sapienza, ESA Advanced Concepts Team ABSTRACT Relative motion

More information

Boundary-Value Problems for Gravimetric Determination of a Precise Geoid

Boundary-Value Problems for Gravimetric Determination of a Precise Geoid Zdenek Martinec Boundary-Value Problems for Gravimetric Determination of a Precise Geoid With 51 Figures and 3 Tables Springer List of symbols Acknowledgements ix xii Introduction 1 1 The Stokes two-boundary-value

More information

Frank Y. Wang. Physics with MAPLE. The Computer Algebra Resource for Mathematical Methods in Physics. WILEY- VCH WILEY-VCH Verlag GmbH & Co.

Frank Y. Wang. Physics with MAPLE. The Computer Algebra Resource for Mathematical Methods in Physics. WILEY- VCH WILEY-VCH Verlag GmbH & Co. Frank Y. Wang Physics with MAPLE The Computer Algebra Resource for Mathematical Methods in Physics WILEY- VCH WILEY-VCH Verlag GmbH & Co. KGaA k Preface Guide for Users Bibliography XI XVII XIX 1 Introduction

More information

SPECIAL FUNCTIONS OF MATHEMATICS FOR ENGINEERS

SPECIAL FUNCTIONS OF MATHEMATICS FOR ENGINEERS SPECIAL FUNCTIONS OF MATHEMATICS FOR ENGINEERS Second Edition LARRY C. ANDREWS OXFORD UNIVERSITY PRESS OXFORD TOKYO MELBOURNE SPIE OPTICAL ENGINEERING PRESS A Publication of SPIE The International Society

More information

Symplectic Correctors for Canonical Heliocentric N-Body Maps

Symplectic Correctors for Canonical Heliocentric N-Body Maps Symplectic Correctors for Canonical Heliocentric N-Body Maps J. Wisdom Massachusetts Institute of Technology, Cambridge, MA 02139 wisdom@poincare.mit.edu Received ; accepted 2 ABSTRACT Symplectic correctors

More information

CALCULATION OF POSITION AND VELOCITY OF GLONASS SATELLITE BASED ON ANALYTICAL THEORY OF MOTION

CALCULATION OF POSITION AND VELOCITY OF GLONASS SATELLITE BASED ON ANALYTICAL THEORY OF MOTION ARTIFICIAL SATELLITES, Vol. 50, No. 3 2015 DOI: 10.1515/arsa-2015-0008 CALCULATION OF POSITION AND VELOCITY OF GLONASS SATELLITE BASED ON ANALYTICAL THEORY OF MOTION W. Góral, B. Skorupa AGH University

More information

Satellite Orbital Maneuvers and Transfers. Dr Ugur GUVEN

Satellite Orbital Maneuvers and Transfers. Dr Ugur GUVEN Satellite Orbital Maneuvers and Transfers Dr Ugur GUVEN Orbit Maneuvers At some point during the lifetime of most space vehicles or satellites, we must change one or more of the orbital elements. For example,

More information

FROM ORDERED TO CHAOTIC MOTION IN CELESTIAL MECHANICS

FROM ORDERED TO CHAOTIC MOTION IN CELESTIAL MECHANICS From Ordered to Chaotic Motion in Celestial Mechanics Downloaded from www.worldscientific.com FROM ORDERED TO CHAOTIC MOTION IN CELESTIAL MECHANICS From Ordered to Chaotic Motion in Celestial Mechanics

More information

Spacecraft Dynamics and Control

Spacecraft Dynamics and Control Spacecraft Dynamics and Control Matthew M. Peet Arizona State University Lecture 10: Rendezvous and Targeting - Lambert s Problem Introduction In this Lecture, you will learn: Introduction to Lambert s

More information

Lecture 2c: Satellite Orbits

Lecture 2c: Satellite Orbits Lecture 2c: Satellite Orbits Outline 1. Newton s Laws of Mo3on 2. Newton s Law of Universal Gravita3on 3. Kepler s Laws 4. Pu>ng Newton and Kepler s Laws together and applying them to the Earth-satellite

More information

QUANTUM MECHANICS. Franz Schwabl. Translated by Ronald Kates. ff Springer

QUANTUM MECHANICS. Franz Schwabl. Translated by Ronald Kates. ff Springer Franz Schwabl QUANTUM MECHANICS Translated by Ronald Kates Second Revised Edition With 122Figures, 16Tables, Numerous Worked Examples, and 126 Problems ff Springer Contents 1. Historical and Experimental

More information

NUMERICAL METHODS FOR ENGINEERING APPLICATION

NUMERICAL METHODS FOR ENGINEERING APPLICATION NUMERICAL METHODS FOR ENGINEERING APPLICATION Second Edition JOEL H. FERZIGER A Wiley-Interscience Publication JOHN WILEY & SONS, INC. New York / Chichester / Weinheim / Brisbane / Singapore / Toronto

More information

Mathematica. 1? Birkhauser. Continuum Mechanics using. Fundamentals, Methods, and Applications. Antonio Romano Addolorata Marasco.

Mathematica. 1? Birkhauser. Continuum Mechanics using. Fundamentals, Methods, and Applications. Antonio Romano Addolorata Marasco. Antonio Romano Addolorata Marasco Continuum Mechanics using Mathematica Fundamentals, Methods, and Applications Second Edition TECHNISCHE INFORM ATIONSB IBLIOTHEK UNIVERSITATSBtBLIOTHEK HANNOVER 1? Birkhauser

More information

Solving Problems in Scientific Computing Using Maple and MATLAB 9

Solving Problems in Scientific Computing Using Maple and MATLAB 9 Walter Gander Jiri Hirebicek Solving Problems in Scientific Computing Using Maple and MATLAB 9 Third, Expanded and Revised Edition 1997 With 161 Figures and 12 Tables Springer r Contents Chapter 1. The

More information

Aerodynamic Lift and Drag Effects on the Orbital Lifetime Low Earth Orbit (LEO) Satellites

Aerodynamic Lift and Drag Effects on the Orbital Lifetime Low Earth Orbit (LEO) Satellites Aerodynamic Lift and Drag Effects on the Orbital Lifetime Low Earth Orbit (LEO) Satellites I. Introduction Carlos L. Pulido Department of Aerospace Engineering Sciences University of Colorado Boulder Abstract

More information

EasyChair Preprint. Retrograde GEO Orbit Design Method Based on Lunar Gravity Assist for Spacecraft

EasyChair Preprint. Retrograde GEO Orbit Design Method Based on Lunar Gravity Assist for Spacecraft EasyChair Preprint 577 Retrograde GEO Orbit Design Method Based on Lunar Gravity Assist for Spacecraft Renyong Zhang EasyChair preprints are intended for rapid dissemination of research results and are

More information

The two-body Kepler problem

The two-body Kepler problem The two-body Kepler problem set center of mass at the origin (X = 0) ignore all multipole moments (spherical bodies or point masses) define r := r 1 r 2,r:= r,m:= m 1 + m 2,µ:= m 1 m 2 /m reduces to effective

More information