{"product_id":"fundamental-spacecraft-dynamics-and-control-9781118753538","title":"Fundamental Spacecraft Dynamics and Control","description":"\u003cb\u003eBook Synopsis\u003c\/b\u003e\u003cbr\u003e\u003cp\u003e\u003c\/p\u003e\u003cp\u003e\u003cb\u003eAn extensive text reference includes around an asteroid - a new and important topic\u003c\/b\u003e\u003c\/p\u003e \u003cul\u003e\n\u003cli\u003eCovers the most updated contents in spacecraft dynamics and control, both in theory and application\u003c\/li\u003e\n\u003cli\u003eIntroduces the application to motion around asteroids - a new and important topic\u003c\/li\u003e\n\u003cli\u003eWritten by a very experienced researcher in this area\u003c\/li\u003e\n\u003c\/ul\u003e\u003cbr\u003e\u003cbr\u003e\u003cb\u003eTrade Review\u003c\/b\u003e\u003cbr\u003e\u003cp\u003e“I consider this text a valuable addition to the library of both the student and the practitioner. I know of no other text that follows the unique and innovative approach of treating introductory spacecraft dynamics and control by means of vectrix calculus. This book can be considered as a prequel to those wishing to study the more advanced graduate-level text of Hughes.”  (\u003ci\u003eIEEE Control Systems Magazine\u003c\/i\u003e, 1 April 2015)\u003c\/p\u003e \u003cp\u003e \u003c\/p\u003e\u003cbr\u003e\u003cbr\u003e\u003cb\u003eTable of Contents\u003c\/b\u003e\u003cbr\u003e\u003cp\u003ePreface xi\u003c\/p\u003e \u003cp\u003eAcknowledgments xiii\u003c\/p\u003e \u003cp\u003eAbout the Author xv\u003c\/p\u003e \u003cp\u003e\u003cb\u003ePart I Orbital Mechanics\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e\u003cb\u003e1 Introduction 3\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e1.1 History 3\u003c\/p\u003e \u003cp\u003e1.1.1 Kepler’s Laws 3\u003c\/p\u003e \u003cp\u003e1.1.2 Newton’s Laws 4\u003c\/p\u003e \u003cp\u003e1.1.3 Space Missions 5\u003c\/p\u003e \u003cp\u003e1.2 Coordinate Systems 6\u003c\/p\u003e \u003cp\u003e1.2.1 Earth Reference Frame 6\u003c\/p\u003e \u003cp\u003e1.2.2 Sun-centered Frame 8\u003c\/p\u003e \u003cp\u003e1.2.3 Right Ascension-Declination System 8\u003c\/p\u003e \u003cp\u003e1.2.4 Perifocal Coordinate System 9\u003c\/p\u003e \u003cp\u003e1.2.5 Satellite Coordinate System 9\u003c\/p\u003e \u003cp\u003e1.2.6 Topo-centric-horizon Coordinate System 9\u003c\/p\u003e \u003cp\u003e1.3 Time System 10\u003c\/p\u003e \u003cp\u003e1.3.1 Clocks 10\u003c\/p\u003e \u003cp\u003e1.3.2 Time 11\u003c\/p\u003e \u003cp\u003e1.3.3 Reference Motions 14\u003c\/p\u003e \u003cp\u003e1.4 References and Further Reading 16\u003c\/p\u003e \u003cp\u003e1.5 Summary and Keywords 16\u003c\/p\u003e \u003cp\u003eProblems 17\u003c\/p\u003e \u003cp\u003eReferences 17\u003c\/p\u003e \u003cp\u003e\u003cb\u003e2 Keplerian Motion 19\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e2.1 N-body System 19\u003c\/p\u003e \u003cp\u003e2.2 The Two-body Problem 21\u003c\/p\u003e \u003cp\u003e2.2.1 Geometry for Two Bodies in an Inertial Reference Frame 21\u003c\/p\u003e \u003cp\u003e2.2.2 Relative Motion of Two Bodies 21\u003c\/p\u003e \u003cp\u003e2.2.3 Constants of the Motion 23\u003c\/p\u003e \u003cp\u003e2.2.4 Orbital Path 27\u003c\/p\u003e \u003cp\u003e2.3 Orbital Elements 36\u003c\/p\u003e \u003cp\u003e2.3.1 Kepler’s COEs 36\u003c\/p\u003e \u003cp\u003e2.3.2 Alternate Orbital Element Quantities 38\u003c\/p\u003e \u003cp\u003e2.3.3 A Calculation Example 38\u003c\/p\u003e \u003cp\u003e2.4 Coordinate Transformations 40\u003c\/p\u003e \u003cp\u003e2.4.1 Rotation 41\u003c\/p\u003e \u003cp\u003e2.4.2 From P̂Q̂Ŵ to ÎĴK̂ 41\u003c\/p\u003e \u003cp\u003e2.4.3 From ÎĴK̂ to ŜÊẐ 43\u003c\/p\u003e \u003cp\u003e2.4.4 Single Radar Observation 45\u003c\/p\u003e \u003cp\u003e2.4.5 Summary of the Transformation 48\u003c\/p\u003e \u003cp\u003e2.4.6 Three Position Vectors (Gibbs Method) 50\u003c\/p\u003e \u003cp\u003e2.5 Time of Flight (TOF) 51\u003c\/p\u003e \u003cp\u003e2.5.1 Kepler’s Equation (Elliptical Orbits) 51\u003c\/p\u003e \u003cp\u003e2.5.2 Numerical Solution 53\u003c\/p\u003e \u003cp\u003e2.5.3 Universal Variable X 56\u003c\/p\u003e \u003cp\u003e2.5.4 f and g Expansion 60\u003c\/p\u003e \u003cp\u003e2.6 Summary and Keywords 62\u003c\/p\u003e \u003cp\u003eProblems 63\u003c\/p\u003e \u003cp\u003eReferences 67\u003c\/p\u003e \u003cp\u003e\u003cb\u003e3 Orbit Maneuver 69\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e3.1 Basic Orbital Transfer 69\u003c\/p\u003e \u003cp\u003e3.1.1 In-plane (Coplanar) Changes 69\u003c\/p\u003e \u003cp\u003e3.1.2 Out-of-plane (Non-coplanar) Changes 71\u003c\/p\u003e \u003cp\u003e3.1.3 The Phase Angle 72\u003c\/p\u003e \u003cp\u003e3.2 Ballistic Missiles 73\u003c\/p\u003e \u003cp\u003e3.2.1 Ballistic Missile Trajectory 74\u003c\/p\u003e \u003cp\u003e3.2.2 Effect of the Earth’s Rotation 77\u003c\/p\u003e \u003cp\u003e3.3 Lunar Missions 80\u003c\/p\u003e \u003cp\u003e3.3.1 Possibility of Transfer 80\u003c\/p\u003e \u003cp\u003e3.3.2 More Practical Scenario 83\u003c\/p\u003e \u003cp\u003e3.4 Interplanetary Travel 87\u003c\/p\u003e \u003cp\u003e3.4.1 Sphere of Influence (SOI) 88\u003c\/p\u003e \u003cp\u003e3.4.2 Scenario 89\u003c\/p\u003e \u003cp\u003e3.4.3 Gravity Assist 93\u003c\/p\u003e \u003cp\u003e3.5 Launch Issues, Starting the Mission 96\u003c\/p\u003e \u003cp\u003e3.5.1 Launch Time 96\u003c\/p\u003e \u003cp\u003e3.5.2 When and Where to Launch 97\u003c\/p\u003e \u003cp\u003e3.5.3 Launch Velocity 98\u003c\/p\u003e \u003cp\u003e3.5.4 Rockets and Launch Vehicles 100\u003c\/p\u003e \u003cp\u003e3.5.5 Reentry 101\u003c\/p\u003e \u003cp\u003e3.6 Summary and Keywords 102\u003c\/p\u003e \u003cp\u003eProblems 102\u003c\/p\u003e \u003cp\u003eReferences 106\u003c\/p\u003e \u003cp\u003e\u003cb\u003e4 Special Topics 107\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e4.1 Relative Motion – CW Equation 107\u003c\/p\u003e \u003cp\u003e4.1.1 Equations of Motion 107\u003c\/p\u003e \u003cp\u003e4.1.2 Examples 110\u003c\/p\u003e \u003cp\u003e4.1.3 J\u003csub\u003e2\u003c\/sub\u003e Perturbed No-circular Target Orbit 112\u003c\/p\u003e \u003cp\u003e4.2 Lambert Problem 113\u003c\/p\u003e \u003cp\u003e4.2.1 Lambert’s Theorem 114\u003c\/p\u003e \u003cp\u003e4.2.2 Culp’s Proof of Lambert’s Theorem 117\u003c\/p\u003e \u003cp\u003e4.2.3 f , g Function Algorithm 119\u003c\/p\u003e \u003cp\u003e4.2.4 Examples 120\u003c\/p\u003e \u003cp\u003e4.2.5 Comparison of CW and Nonlinear Lambert Analysis 122\u003c\/p\u003e \u003cp\u003e4.3 Orbit Determination 123\u003c\/p\u003e \u003cp\u003e4.4 Optimal Control 127\u003c\/p\u003e \u003cp\u003e4.5 Three-Body Problem – CRTBP 132\u003c\/p\u003e \u003cp\u003e4.5.1 Equations of Motion 134\u003c\/p\u003e \u003cp\u003e4.5.2 Lagrange Points 135\u003c\/p\u003e \u003cp\u003e4.5.3 Examples of CRTBP 137\u003c\/p\u003e \u003cp\u003e4.6 Summary and Keywords 139\u003c\/p\u003e \u003cp\u003eProblems 141\u003c\/p\u003e \u003cp\u003eReferences 145\u003c\/p\u003e \u003cp\u003e\u003cb\u003e5 Perturbed Orbital Motions 147\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e5.1 Special Perturbation 147\u003c\/p\u003e \u003cp\u003e5.1.1 General Concept of Perturbation 147\u003c\/p\u003e \u003cp\u003e5.1.2 Cowell’s Method 148\u003c\/p\u003e \u003cp\u003e5.1.3 Encke’s Method 148\u003c\/p\u003e \u003cp\u003e5.1.4 Variation of Parameters (COEs) 149\u003c\/p\u003e \u003cp\u003e5.2 Systematic Method to Derive VOP 151\u003c\/p\u003e \u003cp\u003e5.2.1 Variation of Orbital Elements 151\u003c\/p\u003e \u003cp\u003e5.2.2 Variation of r and 𝑣 156\u003c\/p\u003e \u003cp\u003e5.3 General Perturbations (GA) 157\u003c\/p\u003e \u003cp\u003e5.3.1 An Example of GP 158\u003c\/p\u003e \u003cp\u003e5.3.2 General Perturbation Techniques 158\u003c\/p\u003e \u003cp\u003e5.3.3 Total Perturbation 161\u003c\/p\u003e \u003cp\u003e5.3.4 Analytical Perturbation Formulation 162\u003c\/p\u003e \u003cp\u003e5.3.5 Gravity Potential 165\u003c\/p\u003e \u003cp\u003e5.4 Numerical Methods 168\u003c\/p\u003e \u003cp\u003e5.5 Summary and Keywords 169\u003c\/p\u003e \u003cp\u003eProblems 169\u003c\/p\u003e \u003cp\u003eReferences 171\u003c\/p\u003e \u003cp\u003e\u003cb\u003e6 Orbital Motion Around Asteroids 173\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e6.1 Introduction 173\u003c\/p\u003e \u003cp\u003e6.2 Problem Formulation 174\u003c\/p\u003e \u003cp\u003e6.3 Motion Equations 177\u003c\/p\u003e \u003cp\u003e6.4 Progress and Some Conclusions 178\u003c\/p\u003e \u003cp\u003e6.4.1 Secular Motion 178\u003c\/p\u003e \u003cp\u003e6.4.2 Resonance 180\u003c\/p\u003e \u003cp\u003e6.4.3 Periodic Orbits 180\u003c\/p\u003e \u003cp\u003e6.5 Conclusions 182\u003c\/p\u003e \u003cp\u003e6.6 Summary and Keywords 182\u003c\/p\u003e \u003cp\u003eAcknowledgments 183\u003c\/p\u003e \u003cp\u003eProblems 183\u003c\/p\u003e \u003cp\u003eReferences 183\u003c\/p\u003e \u003cp\u003e\u003cb\u003e7 Application 185\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e7.1 Two Line Elements (TLE) 185\u003c\/p\u003e \u003cp\u003e7.2 GPS RINEX 187\u003c\/p\u003e \u003cp\u003e7.2.1 Distribution of Ephemerides 187\u003c\/p\u003e \u003cp\u003e7.2.2 A GPS RINEX Navigation File 188\u003c\/p\u003e \u003cp\u003e7.3 Remote Observation 188\u003c\/p\u003e \u003cp\u003e7.3.1 Orbital Coverage 188\u003c\/p\u003e \u003cp\u003e7.3.2 Ground Track 189\u003c\/p\u003e \u003cp\u003e7.3.3 Ground Station 193\u003c\/p\u003e \u003cp\u003e7.4 Summary and Keywords 196\u003c\/p\u003e \u003cp\u003eProblems 198\u003c\/p\u003e \u003cp\u003eReferences 198\u003c\/p\u003e \u003cp\u003e\u003cb\u003ePart II Attitude Dynamics\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e\u003cb\u003e8 Rigid Body Kinematics 201\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e8.1 Attitude Notions 201\u003c\/p\u003e \u003cp\u003e8.1.1 Attitude 201\u003c\/p\u003e \u003cp\u003e8.1.2 Frames 202\u003c\/p\u003e \u003cp\u003e8.1.3 Vector 204\u003c\/p\u003e \u003cp\u003e8.2 Attitude Parameters 205\u003c\/p\u003e \u003cp\u003e8.2.1 Direct Cosine Matrix 205\u003c\/p\u003e \u003cp\u003e8.2.2 Euler Angles 207\u003c\/p\u003e \u003cp\u003e8.3 Differential Equations of Kinematics 210\u003c\/p\u003e \u003cp\u003e8.3.1 Typical Problem Involving Angular Velocity and Attitude 213\u003c\/p\u003e \u003cp\u003e8.4 Euler’s Theorem 214\u003c\/p\u003e \u003cp\u003e8.4.1 Another Four-Parameter Set 215\u003c\/p\u003e \u003cp\u003e8.4.2 Summary and Extension of Kinematics Notation 216\u003c\/p\u003e \u003cp\u003e8.5 Attitude Determination 219\u003c\/p\u003e \u003cp\u003e8.5.1 Sensors 219\u003c\/p\u003e \u003cp\u003e8.5.2 Attitude Determination 222\u003c\/p\u003e \u003cp\u003e8.6 Summary and Keywords 228\u003c\/p\u003e \u003cp\u003eProblems 228\u003c\/p\u003e \u003cp\u003eReferences 230\u003c\/p\u003e \u003cp\u003e\u003cb\u003e9 Attitude Dynamics 231\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e9.1 Rigid Body Models 231\u003c\/p\u003e \u003cp\u003e9.1.1 Particle Model 232\u003c\/p\u003e \u003cp\u003e9.1.2 Continuous Model 232\u003c\/p\u003e \u003cp\u003e9.1.3 Angular Momentum 236\u003c\/p\u003e \u003cp\u003e9.2 Inertia Tensor 238\u003c\/p\u003e \u003cp\u003e9.2.1 Calculation of Inertia Tensor (\u003cb\u003e𝐈\u003c\/b\u003e) 238\u003c\/p\u003e \u003cp\u003e9.2.2 Parallel Axis Theorem (PAT) 240\u003c\/p\u003e \u003cp\u003e9.2.3 Change of Vector Basis Theorem 242\u003c\/p\u003e \u003cp\u003e9.2.4 Inertia with a Rotating Panel 244\u003c\/p\u003e \u003cp\u003e9.3 Equation of S\/C Motion 245\u003c\/p\u003e \u003cp\u003e9.3.1 Angular Momentum Principle 245\u003c\/p\u003e \u003cp\u003e9.3.2 Rotational Equation of Motion 246\u003c\/p\u003e \u003cp\u003e9.3.3 Coupled Equations of Motion 247\u003c\/p\u003e \u003cp\u003e9.4 Euler’s Equation 247\u003c\/p\u003e \u003cp\u003e9.4.1 Axisymmetric, Torque-Free Rigid Body 248\u003c\/p\u003e \u003cp\u003e9.4.2 Axisymmetric, Torque-Free Rigid Body Summary 252\u003c\/p\u003e \u003cp\u003e9.4.3 Asymmetric, Torque-Free Rigid Body 253\u003c\/p\u003e \u003cp\u003e9.5 Summary and Keywords 255\u003c\/p\u003e \u003cp\u003eProblems 255\u003c\/p\u003e \u003cp\u003eReferences 255\u003c\/p\u003e \u003cp\u003e\u003cb\u003e10 Attitude Stabilization and Control 257\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e10.1 Free Body Motion Stability 257\u003c\/p\u003e \u003cp\u003e10.2 Dual-Spin Stabilization 259\u003c\/p\u003e \u003cp\u003e10.3 Gravity Gradient Stabilization 260\u003c\/p\u003e \u003cp\u003e10.4 Three-axis Stabilization 263\u003c\/p\u003e \u003cp\u003e10.5 Complete Dynamical Modeling of Spacecraft 266\u003c\/p\u003e \u003cp\u003e10.5.1 Flexible Panels Example 267\u003c\/p\u003e \u003cp\u003e10.5.2 Liquid Sloshing Example 268\u003c\/p\u003e \u003cp\u003e10.5.3 A Mass Spring S\/C Example 268\u003c\/p\u003e \u003cp\u003e10.6 Summary and Keywords 269\u003c\/p\u003e \u003cp\u003eProblems 269\u003c\/p\u003e \u003cp\u003eReferences 271\u003c\/p\u003e \u003cp\u003e\u003cb\u003eAppendix A Math Review 273\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003eA.1 Power, Taylor Series 273\u003c\/p\u003e \u003cp\u003eA.2 Differential Correction 276\u003c\/p\u003e \u003cp\u003eAlgorithm Process 277\u003c\/p\u003e \u003cp\u003eA.3 Spherical Trigonometry 278\u003c\/p\u003e \u003cp\u003eA.4 Summary and Keywords 281\u003c\/p\u003e \u003cp\u003eReferences 281\u003c\/p\u003e \u003cp\u003eIndex 283\u003c\/p\u003e","brand":"John Wiley \u0026 Sons Inc","offers":[{"title":"Default Title","offer_id":49406916297047,"sku":"9781118753538","price":90.25,"currency_code":"GBP","in_stock":false}],"url":"https:\/\/bookcurl.com\/products\/fundamental-spacecraft-dynamics-and-control-9781118753538","provider":"Book Curl","version":"1.0","type":"link"}