On-orbit real-time magnetometer bias determination for micro-satellites without attitude information
Due to the disadvantages such as complex calculation, low accuracy of estimation, and being non real time in present methods, a new real-time algorithm is developed for on-orbit mag- netometer bias determination of micro-satellites without attitude knowledge in this paper. This method uses the diffe...
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          | Published in | Chinese journal of aeronautics Vol. 28; no. 5; pp. 1503 - 1509 | 
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| Main Authors | , , | 
| Format | Journal Article | 
| Language | English | 
| Published | 
            Elsevier Ltd
    
        01.10.2015
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| Subjects | |
| Online Access | Get full text | 
| ISSN | 1000-9361 2588-9230  | 
| DOI | 10.1016/j.cja.2015.08.001 | 
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| Abstract | Due to the disadvantages such as complex calculation, low accuracy of estimation, and being non real time in present methods, a new real-time algorithm is developed for on-orbit mag- netometer bias determination of micro-satellites without attitude knowledge in this paper. This method uses the differential value approach. It avoids the impact of quartic nature and uses the iterative method to satisfy real-time applications. Simulation results indicate that the new real-time algorithm is more accurate compared with other methods, which are also tested by an experiment system using real noise data. With the new real-time algorithm, a magnetometer calibration can be taken on-orbit and will reduce the demand for computing power effectively. | 
    
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| AbstractList | Due to the disadvantages such as complex calculation, low accuracy of estimation, and being non real time in present methods, a new real-time algorithm is developed for on-orbit mag- netometer bias determination of micro-satellites without attitude knowledge in this paper. This method uses the differential value approach. It avoids the impact of quartic nature and uses the iterative method to satisfy real-time applications. Simulation results indicate that the new real-time algorithm is more accurate compared with other methods, which are also tested by an experiment system using real noise data. With the new real-time algorithm, a magnetometer calibration can be taken on-orbit and will reduce the demand for computing power effectively. Due to the disadvantages such as complex calculation, low accuracy of estimation, and being non real time in present methods, a new real-time algorithm is developed for on-orbit magnetometer bias determination of micro-satellites without attitude knowledge in this paper. This method uses the differential value approach. It avoids the impact of quartic nature and uses the iterative method to satisfy real-time applications. Simulation results indicate that the new real-time algorithm is more accurate compared with other methods, which are also tested by an experiment system using real noise data. With the new real-time algorithm, a magnetometer calibration can be taken on-orbit and will reduce the demand for computing power effectively.  | 
    
| Author | Zhang Zhen Xiong Jianping Jin Jin | 
    
| AuthorAffiliation | Department of Precision Instrument. Tsinghua University, Beijing 100084. China Space Center, Tsinghua University, Beijing 100084, China | 
    
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| CitedBy_id | crossref_primary_10_1016_j_cja_2019_08_011 crossref_primary_10_1109_JSEN_2024_3370624 crossref_primary_10_1016_j_ifacol_2020_12_1948 crossref_primary_10_1016_j_isatra_2016_01_012 crossref_primary_10_1016_j_asr_2022_09_021 crossref_primary_10_1016_j_measurement_2017_10_017 crossref_primary_10_1007_s40295_022_00349_5  | 
    
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| Keywords | Attitude-independent Magnetometer bias Micro-satellite Real-time On-orbit determination  | 
    
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| Notes | Magnetometer bias:On-orbit determinationMicro-satellite;Attitude-independent;Real-time 11-1732/V Due to the disadvantages such as complex calculation, low accuracy of estimation, and being non real time in present methods, a new real-time algorithm is developed for on-orbit mag- netometer bias determination of micro-satellites without attitude knowledge in this paper. This method uses the differential value approach. It avoids the impact of quartic nature and uses the iterative method to satisfy real-time applications. Simulation results indicate that the new real-time algorithm is more accurate compared with other methods, which are also tested by an experiment system using real noise data. With the new real-time algorithm, a magnetometer calibration can be taken on-orbit and will reduce the demand for computing power effectively.  | 
    
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| SubjectTerms | Attitude-independent Magnetometer bias Micro-satellite On-orbit determination Real-time 估计精度 偏置 姿态信息 实时算法 微卫星 磁力计 计算能力 非实时  | 
    
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