Real-Time Attitude Independent Calibration of Spinning Spacecraft Magnetometers Using Quasi-Measurements

Date

2022-11-01

Author

Cetin, Mustafa Efe
Söken, Halil Ersin
Sakai, Shin-ichiro

Metadata

Show full item record

This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

Item Usage Stats

117
views

0
downloads

Magnetometers are essential sensors for attitude estimation in small spacecraft due to their robust, inexpensive, and lightweight characteristics. However, the raw measurements contain sensor errors. These errors degrade the attitude estimation accuracy. This study proposes a complete real-time attitude-independent magnetometer calibration algorithm for spinning spacecraft. The recursive algorithm aims to estimate the full error state, bias, scale factor, and non-orthogonality corrections in real-time and without any attitude information. The well-known attitude-independent observation based on the magnitude of the sensed magnetic field is aided by newly introduced quasi-measurements to build the algorithm. The algorithm is tested with both simulations and actual spacecraft data. Four quasi-measurements, which are derived using dynamic characteristics of the spacecraft, considerably improve the convergence characteristics of the filter and the estimation accuracy.

Subject Keywords

Magnetometer calibration, Quasi-measurements, Spinning spacecraft, Unscented Kalman filter

URI

https://hdl.handle.net/11511/101587

Journal

JOURNAL OF THE ASTRONAUTICAL SCIENCES

DOI

https://doi.org/10.1007/s40295-022-00349-5

Collections

Department of Aerospace Engineering, Article

Suggestions

OpenMETU
Core

Realtime Magnetometer Calibration for Spinning Aerospace Vehicles Çetin, Mustafa Efe; Söken, Halil Ersin; Tekinalp, Ozan; Department of Aerospace Engineering (2022-2-8) Magnetometers are essential sensors for attitude estimation application in small spacecrafts due to their robust, inexpensive and lightweight characteristics. However, their direct usage is not applicable due to sensor errors. These errors limit the overall attitude estimation accuracy. This study proposes a complete real-time attitude independent magnetometer calibration algorithm for spinning aerospace vehicles. The recursive algorithm aims estimating the complete error state; consisting bias, scale facto...
Spinning Spacecraft Attitude Filtering with Spin Parameters: Performance Evaluation with Real Data Söken, Halil Ersin; Van Der Ha, Jozef C. (null; 2017-06-07) Three-axis attitude estimation for spinning spacecraft is recently of considerable practical interest. In this scope, sequential filtering algorithms are also being studied recently. In this study, we extend our recent research for a nonlinear filtering algorithm for spinning spacecraft attitude estimation. In the filter the attitude of the spacecraft is represented using a set of spin parameters. These parameters consist of the spin-axis orientation unit vector in the inertial frame and the spin phase angl...
Fault Tolerant Attitude Estimation for Small Satellites Söken, Halil Ersin (CRC, New York , 2020-12-01) 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 ...
Vision-Based Detection and Distance Estimation of Micro Unmanned Aerial Vehicles Gökçe, Fatih; Üçoluk, Göktürk; Şahin, Erol; Kalkan, Sinan (MDPI, ST ALBAN-ANLAGE 66, CH-4052 BASEL, SWITZERLAND, 2015-9) Detection and distance estimation of micro unmanned aerial vehicles (mUAVs) is crucial for (i) the detection of intruder mUAVs in protected environments; (ii) sense and avoid purposes on mUAVs or on other aerial vehicles and (iii) multi-mUAV control scenarios, such as environmental monitoring, surveillance and exploration. In this article, we evaluate vision algorithms as alternatives for detection and distance estimation of mUAVs, since other sensing modalities entail certain limitations on the environment...
Design of a control moment gyroscope with outer rotor BLDC motor İnce, Berk; Ertan, Hulusi Bülent; Department of Electrical and Electronics Engineering (2019) The aim of this thesis is to design a control moment gyroscope (CMG) with outer rotor BLDC motor for medium size satellites. CMG is a device that provides high output torque to the satellite in order to maneuvering satellites rapidly. CMG is the most efficient actuator in terms of output torque capacity when it is compared with other type actuators such as the reaction wheel. The first step of the designing CMG is to determine CMG design specifications. The mass and volume specifications of the designed CMG...

Citation Formats

M. E. Cetin, H. E. Söken, and S.-i. Sakai, “Real-Time Attitude Independent Calibration of Spinning Spacecraft Magnetometers Using Quasi-Measurements,” JOURNAL OF THE ASTRONAUTICAL SCIENCES, pp. 0–0, 2022, Accessed: 00, 2023. [Online]. Available: https://hdl.handle.net/11511/101587.