- ホーム
- > 洋書
- > 英文書
- > Science / Mathematics
Full Description
Aimed at students, faculty and professionals in the aerospace field, this book provides practical information on the development, analysis, and control of a single and/or multiple spacecraft in space. This book is divided into two major sections: single and multiple satellite motion. The first section analyses the orbital mechanics, orbital perturbations, and attitude dynamics of a single satellite around the Earth. Using the knowledge of a single satellite motion, the translation of a group of satellites called formation flying or constellation is explained. Formation flying has been one of the main research topics over the last few years and this book explains different control approaches to control the satellite attitude motion and/or to maintain the constellation together. The control schemes are explained in the discrete domain such that it can be easily implemented on the computer on board the satellite. The key objective of this book is to show the reader the practical and the implementation process in the discrete domain.
Contents
DedicationList of figuresList of tablesList of symbolsAcknowledgementsPrefaceAbout the authorsChapter 1: Introduction1.1 Introduction to the book1.2 Book divisionChapter 2: Two body orbital motionAbstract:2.1 Introduction to orbital motion2.2 Constraints and generalized coordinates2.3 Lagrange's equation2.4 System of particles2.5 Two body orbital motion problem2.6 Orbital equations of motion2.7 Energy and velocity of orbiting bodies2.8 Escape velocity2.9 Earth Coordinate Inertial (ECI) system2.10 Period of an orbit2.11 Development of Kepler's equation2.12 Suggested problemsChapter 3: Orbital perturbations in the two body motionAbstract:3.1 Introduction to disturbance effects3.2 Lagrange planetary equations3.3 Perturbation due to the earth oblateness3.4 The near-Earth atmosphere effects3.5 Solar radiation pressure force3.6 Other disturbance effects3.7 Suggested problemsChapter 4: Frame rotations and quaternionsAbstract:4.1 Introduction to rotations and quaternions4.2 Two-dimensional frame rotations4.3 Three-dimensional frame rotations4.4 Example of frame rotations4.5 Quaternion definition and rotations4.6 Quaternion to Euler angle relations4.7 Suggested problemsChapter 5: Rigid body motionAbstract:5.1 Introduction to attitude dynamics5.2 Rate of change of a vector5.3 Moment of inertia5.4 Principal moments of inertia5.5 Energy formulation5.6 Rate of change of a quaternion5.7 Ares V equations of motion5.8 Suggested problemsChapter 6: Environmental and actuator torquesAbstract:6.1 Introduction to torque formulation6.2 Environmental torques6.3 Actuator (or control) torques6.4 Suggested problemsChapter 7: Continuous and digital control systemsAbstract:7.1 Introduction to methods of designing continuous and discrete control systems7.2 Ares V equations of motion for first stage flight7.3 Continuous control formulation7.4 Discrete control formulation7.5 Adaptive and intelligent controls7.6 Suggested problemsChapter 8: ExampleAbstract:8.1 Introduction to examples in spacecraft attitude dynamics and control8.2 Nanosatellite problem definition8.3 B-dot controller for fast corrections8.4 Linear quadratic regulator for attitude correction8.5 Linear quadratic regulator control weight design8.6 Suggested problemsChapter 9: Formation flyingAbstract:9.1 Introduction to formation flying9.2 Tschauner-Hempel formulation9.3 Clohessy-Wiltshire formulation9.4 Earth oblateness and solar effects in formation flying9.5 Lawden solution9.6 Discrete optimal control problem for formation flying9.7 Formation flying controller implementation9.8 Suggested problemsChapter 10: Deployment procedure for a constellationAbstract:10.1 Introductory comments10.2 Desired conditions of the satellites in the proposed tetrahedron constellation10.3 Transfer from a circular orbit to the elliptical orbit (stage 1)10.4 Station-keeping procedure (stage 2)10.5 Deployment procedure for the tetrahedron constellation10.6 Remarks10.7 Suggested problemsChapter 11: Reconfiguration procedure for a constellationAbstract:11.1 Introduction to the reconfiguration process of a constellation11.2 Data mining process of the Lagrange planetary equations11.3 Fuzzy logic controller11.4 Phase I to II in-plane motion fuzzy logic control system11.5 Phase II to III in-plane motion fuzzy logic controller11.6 Out-of-plane motion correction11.7 Some solutions for the reconfiguration procedures11.8 Implementation of the fuzzy logic controller11.9 Adaptive control scheme for reconfiguration procedure11.10 Remarks11.11 Suggested problemsAppendix: Formulae relating to orbital mechanicsIndex
