2022
DOI: 10.1016/j.measurement.2022.110734
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Attitude-Induced error modeling and compensation with GRU networks for the polarization compass during UAV orientation

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Cited by 22 publications
(17 citation statements)
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“…A polarized camera (based on Sony sensor IMX250MZR, 2448 × 2048 pixels, 24 fps, such as mentioned in Section 2.2.5 ) was mounted on board a 15 kg six-rotor UAV [ 211 ]. Polarimetric images were processed by gated recurrent unit (GRU) neural network generating an output refresh signal of 10 Hz with a heading accuracy of 0.5°.…”
Section: Polarized Vision For Robotics Navigationmentioning
confidence: 99%
“…A polarized camera (based on Sony sensor IMX250MZR, 2448 × 2048 pixels, 24 fps, such as mentioned in Section 2.2.5 ) was mounted on board a 15 kg six-rotor UAV [ 211 ]. Polarimetric images were processed by gated recurrent unit (GRU) neural network generating an output refresh signal of 10 Hz with a heading accuracy of 0.5°.…”
Section: Polarized Vision For Robotics Navigationmentioning
confidence: 99%
“…Heading errors are increased when the body axis tilt and the solar meridian angle are coupled. Utilizing a GRU neural network, an extensive investigation of attitude angle factors has been performed, creating a brand-new heading error modeling and compensating technique in [109]. In terms of forecasting UAV direction, their solution fared better than cutting-edge algorithms.…”
Section: Recurrent Neural Network (Rnn)mentioning
confidence: 99%
“…The third category is by constructing a sensor model or fusing multiple algorithms, Liu [16] proposed a UAV attitude estimation algorithm considering motion acceleration interference, which improved the accuracy and interference resistance of UAV navigation system attitude estimation in dynamic environment. Zhao [17] proposed a gated recurrent unit (GRU) neural network-based method for modeling and compensating UAV heading errors, which has a good performance in predicting vehicle orientation. Liu [18] proposed an attitude solution algorithm based on acceleration correction model, which can attenuate the interference of non-gravitational acceleration on attitude calculation and avoid attitude angle divergence of aircraft navigation system in dynamic environment.…”
Section: Introductionmentioning
confidence: 99%