TY - GEN
T1 - Comparison of compensation methods on RLG temperature error and their application in POS
AU - Cheng, Junchao
AU - Fang, Jiancheng
PY - 2012
Y1 - 2012
N2 - Motion compensation technology based on Ring Laser Gyroscope (RLG) Position and Orientation System (POS) enormously improves the imaging quality and operation efficiency of airborne remote sensing systems. However, bias error of RLG, aroused by temperature variation, severely deteriorates the measurement precision of POS. To solve this problem, several error modeling and compensation techniques have been devised, including Linear Least Squares Fitting (LLSF), RBF Neural Network (RBF NN) and Least Square Support Vector Machine (LS SVM). Theoretical basis of these methods are introduced. Comparison among them with subjects on model complexity, computing speed, precision and generalization performance is drawn, and conclusions are verified via temperature circling experiment of real RLG. Approach based on LLSF acquires the advantages of high computing speed and low hardware resource occupancy, while superiority on precision and generalization performance of LS SVM is obvious. According to the hostile working environment and high precision requirement of POS, methods based on LLSF and LS SVM are adopted to work under online and offline modes of POS, which meet the demands of computing speed and compensation precision respectively. Airborne flight experiment results demonstrate that, six groups' average online inertial navigation error of RLG POS after 4 hours' flight was 9.5775 nmiles, while the average offline inertial navigation error was 4.0661 nmiles. Such result satisfied the application requirement of high resolution InSAR.
AB - Motion compensation technology based on Ring Laser Gyroscope (RLG) Position and Orientation System (POS) enormously improves the imaging quality and operation efficiency of airborne remote sensing systems. However, bias error of RLG, aroused by temperature variation, severely deteriorates the measurement precision of POS. To solve this problem, several error modeling and compensation techniques have been devised, including Linear Least Squares Fitting (LLSF), RBF Neural Network (RBF NN) and Least Square Support Vector Machine (LS SVM). Theoretical basis of these methods are introduced. Comparison among them with subjects on model complexity, computing speed, precision and generalization performance is drawn, and conclusions are verified via temperature circling experiment of real RLG. Approach based on LLSF acquires the advantages of high computing speed and low hardware resource occupancy, while superiority on precision and generalization performance of LS SVM is obvious. According to the hostile working environment and high precision requirement of POS, methods based on LLSF and LS SVM are adopted to work under online and offline modes of POS, which meet the demands of computing speed and compensation precision respectively. Airborne flight experiment results demonstrate that, six groups' average online inertial navigation error of RLG POS after 4 hours' flight was 9.5775 nmiles, while the average offline inertial navigation error was 4.0661 nmiles. Such result satisfied the application requirement of high resolution InSAR.
KW - Least Square Support Vector Machine
KW - Linear Least Square Fitting
KW - POS
KW - RBF Neural Network
KW - ring laser gyro
KW - temperature error compensation
UR - https://www.scopus.com/pages/publications/84867309654
U2 - 10.1109/ISICT.2012.6291612
DO - 10.1109/ISICT.2012.6291612
M3 - 会议稿件
AN - SCOPUS:84867309654
SN - 9781467326162
T3 - 2012 the 8th IEEE International Symposium on Instrumentation and Control Technology, ISICT 2012 - Proceedings
SP - 189
EP - 194
BT - 2012 the 8th IEEE International Symposium on Instrumentation and Control Technology, ISICT 2012 - Proceedings
T2 - 8th IEEE International Symposium on Instrumentation and Control Technology, ISICT 2012
Y2 - 11 July 2012 through 13 July 2012
ER -