Quan Yonggui, Xiao Tibing, Liu Jianqun, et al. A Method for Correcting Heave Measurement Errors of Attitude Sensors Based on Support Vector Classification[J]. 2025, 42(3): 80-85.
Quan Yonggui, Xiao Tibing, Liu Jianqun, et al. A Method for Correcting Heave Measurement Errors of Attitude Sensors Based on Support Vector Classification[J]. 2025, 42(3): 80-85.DOI: 10.12052/gdutxb.240164.
A Method for Correcting Heave Measurement Errors of Attitude Sensors Based on Support Vector Classification
The precision of attitude sensors in heave compensation systems for floating operations directly affects the compensation accuracy. Mainstream attitude sensors typically achieve a heave measurement accuracy of 5 cm or 5%
which limits the system's ability to r
each a 95% compensation rate. To address this issue
a method based on Support Vector Classification (SVC) was developed to correct measurement errors. The attitude sensor was mounted on a six-degree-of-freedom platform
and the platform's heave displacement
measured by a dynamic capture system
was used as the reference ground truth to determine the sensor's measurement errors. Through significance analysis of the relationship between the errors and the sensor's output signals
three parameters—acceleration
velocity and displacement—were selected as inputs for the SVC model. An SVC model was constructed in MATLAB
and data collected from the system were used for model training and parameter optimization
employing Bayesian optimization and
k
-fold cross-validation techniques. The trained SVC model was then integrated into data acquisition software
with custom code developed to implement classification functions.The results demonstrate that the SVC model effectively identified the error ranges corresponding to the three output parameters of the attitude sensor
enabling specific correction values for each error category. The correction process required an average time of only 1.4 ms. After correction
the root mean square error of the heave displacement decreased from
0.4567
cm to
0.2622
cm (or 2.622% of the amplitude)
while the absolute mean error was reduced from
0.3668
cm to
0.1989
cm. These findings indicate that the proposed method significantly reduces heave measurement errors. Furthermore
the method is applicable for correcting errors in other degrees of freedom outputs of the attitude sensor.
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