Nanosatellites : space and ground technologies, operations and economics /
"Nanosatellites : Space and Ground Technologies, Operations and Economics comprehensively presents the latest research on the fast developing area of nano-satellites. It begins with a brief history of nano-satellites and introduces nano-satellite technologies, payloads for nano-satellite and ex...
Clasificación: | Libro Electrónico |
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Autores principales: | , , |
Formato: | Electrónico eBook |
Idioma: | Inglés |
Publicado: |
Hoboken, NJ :
Wiley,
[2020]
|
Edición: | First edition. |
Temas: | |
Acceso en línea: | Texto completo (Requiere registro previo con correo institucional) |
Tabla de Contenidos:
- Cover
- Title Page
- Copyright
- Contents
- List of Contributors
- Foreword: Nanosatellite Space Experiment
- Introduction by the Editors
- Chapter 1 I-1 A Brief History of Nanosatellites
- 1.1 Introduction
- 1.2 Historical Nanosatellite Launch Rates
- 1.3 The First Nanosatellites
- 1.4 The Large Space Era
- 1.5 The New Space Era
- 1.5.1 Technology Development
- 1.5.2 Commercial Nanosatellites and Constellations
- 1.6 Summary
- References
- Chapter 2 I-2a On-board Computer and Data Handling
- 2.1 Introduction
- 2.2 History
- 2.3 Special Requirements for Space Applications
- 2.4 Hardware
- 2.4.1 Components
- 2.4.2 Brief History of On-board Computers
- 2.4.3 Processors
- 2.4.3.1 Field Programmable Gate Array (FPGA)
- 2.4.4 Mass Memory
- 2.4.5 Bus
- 2.5 Design
- 2.5.1 System Architecture
- 2.5.2 Central Versus Distributed Processing
- 2.5.3 Design Criteria
- 2.5.4 Definition of Requirements
- 2.5.5 Resource Estimation and Data Budget
- 2.5.5.1 Data Budget Analysis
- 2.5.6 Commanding
- 2.5.7 Telemetry
- 2.5.8 Time Generation
- 2.5.9 Handling of Errors
- 2.5.10 Radiation Effects
- References
- Chapter 3 I-2b Operational Systems
- 3.1 Introduction
- 3.2 RTOS Overview
- 3.3 RTOS on On-board Computers (OBCs): Requirements for a Small Satellite
- 3.3.1 Requirements
- 3.4 Example Projects
- 3.5 Conclusions
- References
- Chapter 4 I-2c Attitude Control and Determination
- 4.1 Introduction
- 4.2 ADCS Fundamentals
- 4.3 ADCS Requirements and Stabilization Methods
- 4.4 ADCS Background Theory
- 4.4.1 Coordinate Frame Definitions
- 4.4.2 Attitude Kinematics
- 4.4.3 Attitude Dynamics
- 4.5 Attitude and Angular Rate Determination
- 4.5.1 TRIAD Quaternion Determination
- 4.5.2 Kalman Rate Estimator
- 4.5.2.1 System Model
- 4.5.2.2 Measurement Model
- 4.5.3 Full-State Extended Kalman Filter Estimator
- 4.6 Attitude and Angular Rate Controllers
- 4.6.1 Detumbling Magnetic Controllers
- 4.6.2 Y-Momentum Wheel Controller
- 4.6.3 Three-axis Reaction Wheel Controller
- 4.7 ADCS Sensor and Actuator Hardware
- 4.7.1 Three-Axis Magnetometers
- 4.7.2 Sun Sensors
- 4.7.3 Star Trackers
- 4.7.4 MEMS Rate Sensors
- 4.7.5 Magnetorquers
- 4.7.6 Reaction/Momentum Wheels
- 4.7.7 Orbit Control Sensors and Actuators
- 4.7.8 Integrated ADCS Modules
- References
- Chapter 5 I-2d Propulsion Systems
- 5.1 Introduction
- 5.2 Propulsion Elements
- 5.3 Key Elements in the Development of Micropropulsion Systems
- 5.4 Propulsion System Technologies
- 5.4.1 Chemical Propulsion Technologies
- 5.4.1.1 Cold Gas Thruster
- 5.4.1.2 Monopropellant Engines
- 5.4.1.3 Bipropellant Engines
- 5.4.1.4 Solid Propellant Engines
- 5.4.2 Electric Propulsion Technologies
- 5.4.2.1 Resistojet
- 5.4.2.2 Gridded Ion Engine (GIE)
- 5.4.2.3 Hall Effect Thruster
- 5.4.2.4 Pulsed Plasma Thruster (PPT) and Vacuum Arc Thruster (VAT)
- 5.4.2.5 Colloid/Electrospray and Field-emission Thruster
- 5.5 Mission Elements