Robust double gain unscented Kalman filter for small satellite attitude estimation

Lu Cao; Weiwei Yang; Hengnian Li; Zhidong Zhang; Jianjun Shi

doi:10.1016/j.asr.2017.03.014

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Robust double gain unscented Kalman filter for small satellite attitude estimation

Lu Cao Weiwei Yang Hengnian Li Zhidong Zhang Jianjun Shi

Year: 2017 Journal: Advances in Space Research Vol: 60 (3)Pages: 499-512 Publisher: Elsevier BV

DOI: 10.1016/j.asr.2017.03.014

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Keywords:

Kalman filter Computer science Residual Robustness (evolution) Control theory (sociology) A priori and a posteriori Extended Kalman filter Unscented transform Satellite Observational error Invariant extended Kalman filter Algorithm Mathematics Control (management) Artificial intelligence Engineering Statistics

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Inertial Sensor and Navigation

Physical Sciences → Engineering → Aerospace Engineering

Target Tracking and Data Fusion in Sensor Networks

Physical Sciences → Computer Science → Artificial Intelligence

GNSS positioning and interference

Physical Sciences → Engineering → Aerospace Engineering

Robust double gain unscented Kalman filter for small satellite attitude estimation

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