Table of Contents
PART 1 BASIC MECHANICS
Chapter 1 Particle Kinematics
Chapter 2 Newtonian Mechanics
Chapter 3 Rigid Body Kinematics
Chapter 4 Eulerian Mechanics
Chapter 5 Generalized Methods of Analytical Dynamics
Chapter 6 Variational Methods in Analytical Dynamics
Chapter 7 Hamilton's Generalized Formulations of Analytical Dynamics
Chapter 8 Nonlinear Spacecraft Stability and Control
PART 2 CELESTIAL MECHANICS
Chapter 9 Classical Two-Body Problem
Chapter 10 Restricted Three-Body Problem
Chapter 11 Gravitational Potential Field Models
Chapter 12 Perturbation Methods
Chapter 13 Transfer Orbits
Chapter 14 Spacecraft Formation Flying
Appendix A Transport Theorem Derivation Using Linear Algebra
Appendix B Various Euler Angle Transformations
Appendix C MRP Identity Proof
Appendix D Conic Section Transformations
Appendix E Numerical Subroutines Library
Appendix F First-Order Mapping Between Mean and Osculating Orbit Elements
Appendix G Direct Linear Mapping Between Cartesian Hill Frame Coordinates and Orbit Element Differences
Appendix H Hamel Coefficients for the Rotational Motion of a Rigid Body
Appendix I MRP Kalman Filter
Index
Supporting Materials
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John L. Junkins is Distinguished Professor of Aerospace Engineering at Texas A&M University and holds the Royce E. Wisenbaker Chair. He is Founding Director of the Texas A&M University Institute for Advanced Study. Interests include analytical dynamics, estimation, and control. A prolific author and academic mentor, his awards and honors include AIAA's Guidance, Navigation, and Control Award and the ICCES Lifetime Achievement Medal. He is an Honorary Fellow of AIAA and a graduate of Auburn University and UCLA.
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