Fault Tolerant Attitude Estimation for Small Satellites
Auteurs : Hajiyev Chingiz, Soken Halil Ersin
Small satellites use commercial off-the-shelf sensors and actuators for attitude determination and control (ADC) to reduce the cost. These sensors and actuators are usually not as robust as the available, more expensive, space-proven equipment. As a result, the ADC system of small satellites is more vulnerable to any fault compared to a system for larger competitors. This book aims to present useful solutions for fault tolerance in ADC systems of small satellites. The contents of the book can be divided into two categories: fault tolerant attitude filtering algorithms for small satellites and sensor calibration methods to compensate the sensor errors. MATLAB® will be used to demonstrate simulations.
- Presents fault tolerant attitude estimation algorithms for small satellites with an emphasis on algorithms? practicability and applicability
- Incorporates fundamental knowledge about the attitude determination methods at large
- Discusses comprehensive information about attitude sensors for small satellites
- Reviews calibration algorithms for small satellite magnetometers with simulated examples
- Supports theory with MATLAB simulation results which can be easily understood by individuals without a comprehensive background in this field
- Covers up-to-date discussions for small satellite attitude systems design
Dr. Chingiz Hajiyev is a professor at the Faculty of Aeronautics and Astronautics, Istanbul Technical University (Istanbul, Turkey).
Dr. Halil Ersin Soken is an assistant professor at the Aerospace Engineering Department, Middle East Technical University (Ankara, Turkey).
1. Attitude Parameters.
2. Mathematical Models For Small Satellite Attitude Dynamics and Kinematics.
3. Attitude Sensors.
4. Attitude Sensor Measurement Models.
5. Attitude Determination Using Two Vector Measurements – TRIAD Method.
6. Statistical Methods For Three-Axis Attitude Determination.
7. Kalman Filtering.
8. Adaptive Kalman Filtering.
9. Kalman Filtering for Small Satellite Attitude Estimation.
10. Integration of Single-Frame Methods With Filtering Algorithms For Attitude Estimation.
11. Active Fault Tolerant Attitude Estimation.
12. Fault Tolerant Attitude Estimation: R-Adaptation Methods.
13. Fault Tolerant Attitude Estimation: Q-Adaptation Methods.
14. Integration of R- and Q-Adaptation Methods.
15. In-Orbit Calibration Of Small Satellite Magnetometers: Batch Calibration Algorithms.
16. In-Orbit Calibration Of Small Satellite Magnetometers: Recursive Calibration Algorithms.
Index
Dr. Chingiz Hajiyev is a professor at the Faculty of Aeronautics and Astronautics, Istanbul Technical University (Istanbul, Turkey).
Dr. Halil Ersin Soken is an assistant professor at the Aerospace Engineering Department, Middle East Technical University (Ankara, Turkey).
Date de parution : 09-2023
15.6x23.4 cm
Date de parution : 12-2020
15.6x23.4 cm
Thèmes de Fault Tolerant Attitude Estimation for Small Satellites :
Mots-clés :
Attitude parameters, Euler Angles, The External Disturbance Torques, Solar Radiation Torques, Small Satellite Kinematics, The Internatinal Geomagnetic Reference Field Model, The Earth Magnetic Field Model, Sun Sensor Measurement Model, Gyroscopes, Davenport’s q-Method, Quaternion Estimation Method (QUEST), SVD Method, Kalman Filtering, IN-FLIGHT CALIBRATION, External Disturbance Torques, Attitude determination and control system, Attitude Quaternion, MATLAB, Unscented Kalman Filter Algorithm, Fault tolerant attitude filtering algorithms, Small Satellite, Small satellites, Kalman Filter, Sensor calibration methods, Attitude Estimation, Magnetometer Measurements, Process Noise Covariance, Sun Sensor, UKF, Gyro Bias, Measurement Noise Covariance, Robust Kalman Filters, Noise Covariance, Attitude Filter, Measurement Noise Covariance Matrix, Attitude Error, Accurate Estimation Results, Euler Angles, Gyro Measurements, Filtering Algorithms, Roll Angle Estimation, Sigma Points, Disturbance Torques, Estimate Time Variable Parameters