| Description |
1 online resource (xviii, 170 pages) : illustrations, charts |
| Physical Medium |
polychrome |
| Description |
text file |
| Bibliography |
Includes bibliographical references and index. |
| 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. |
| Local Note |
eBooks on EBSCOhost EBSCO eBook Subscription Academic Collection - North America |
| Subject |
Nanosatellites -- Attitude control systems.
|
|
Nanosatellites -- Attitude control systems. |
|
Nanosatellites -- Mathematical models.
|
|
Nanosatellites. |
|
Mathematical models. |
|
TECHNOLOGY & ENGINEERING -- Engineering (General) |
|
Aerospace & aviation technology. |
|
Automatic control engineering. |
|
Space science. |
| Genre/Form |
Electronic books.
|
| Other Form: |
Print version: Mahdi, Mohammed Chessab. Attitude stablization for CubeSat. Newcastle upon Tyne, UK : Cambridge Scholars Publishing, 2018 1527506517 (OCoLC)1019752341 |
| ISBN |
9781527521636 (electronic book) |
|
152752163X (electronic book) |
|
1527506517 |
|
9781527506510 |
|
