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Book Cover
E-book
Author Mahdi, Mohammed Chessab, author

Title Attitude stablization for CubeSat : concepts and technology / by Mohammed Chessab Mahdi
Published Newcastle upon Tyne, UK : Cambridge Scholars Publishing, 2018
©2018

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Description 1 online resource (xviii, 170 pages) : illustrations, charts
Contents Intro; Table of Contents; List of Symbols; List of Illustrations; List of Tables; Preface; Acronyms and Abbreviations; Chapter One; 1.1 Introduction; 1.2 CubeSat systems; 1.3 Orbital Dynamics; 1.4 Earth's Magnetic Field; 1.5 Launching Facility; 1.6 Poly Picosatellite Orbital Deployer; 1.7 CubeSat Form Factor; 1.8 Attitude Determination and Control System (ADCS); References; Chapter Two; 2.1 Introduction; 2.2 Attitude Stabilization of Sp; 2.3 Passive Attitude Stabilization; 2.4 Active Attitude Stabilization; 2.5 Mode of Attitude Stabilization of a Spacecraft; References; Chapter Three
3.1 Introduction3.2 Reference Frames; 3.3 Dynamic Model; 3.4 Linearized Dynamic Model; 3.5 Disturbance Torques; 3.6 Complete Linearized Mathematical; 3.7 Test for Satellite's Motions; 3.8 State Space Modeling; References; Chapter Four; 4.1 Introduction; 4.2 Control Techniques; 4.3 The Proportional, Integral and Derivative; 4.4 Linear Quadratic Regulator; 4.5 Fuzzy Logic; 4.6 Fuzzy Logic Control; 4.7 Fuzzy Controller Design; 4.8 Fuzzy Logic Attitude Control; 4.9 Three-axis Fuzzy Controller Design; 4.10 Fuzzy Logic Controller Config; References; Chapter Five; 5.1 Introduction
5.2 PID Controller5.3 LQR controller; 5.4 Fuzzy Controller; 5.5 Comparison Between the Three Control Techniques; 5.6 Stability Problem Discussion; 5.7 Notes About Fuzzy Logic Controller; References; Appendix A; A.1 Introduction; A.2 Direction Cosine Matrix; Appendix B; B.1 Coil Design; B.2 American Wire Gauge; Appendix C; C.1 Initialization file for the CubeSat model; C.2 PID Controller Simulation Diagram; C.3 FLC Controller Simulation Diagram; Appendix D; D.1 The International Geomagnetic Reference Field; Index
Summary This book explores CubeSat technology, and develops a nonlinear mathematical model of a spacecraft with the assumption that the satellite is a rigid body. It places emphasis on the CubeSat subsystem, orbit dynamics and perturbations, the satellite attitude dynamic and modeling, and components of attitude determination and the control subsystem. The book focuses on the attitude stabilization methods of spacecraft, and presents gravity gradient stabilization, aerodynamic stabilization, and permanent magnets stabilization as passive stabilization methods, and spin stabilization and three axis stab
Bibliography Includes bibliographical references and index
Notes Print version record
Subject Nanosatellites -- Attitude control systems.
Nanosatellites -- Mathematical models
Aerospace & aviation technology.
Automatic control engineering.
Space science.
TECHNOLOGY & ENGINEERING -- Engineering (General)
Nanosatellites -- Attitude control systems
Form Electronic book
ISBN 9781527521636
152752163X