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Attitude stablization for CubeSat : concepts and technology /

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 att...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Mahdi, Mohammed Chessab (Autor)
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Newcastle upon Tyne, UK : Cambridge Scholars Publishing, 2018.
Temas:
Acceso en línea:Texto completo
Tabla de Contenidos:
  • 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