DocumentCode
724098
Title
Data pre-processing of inertial measurement unit based on abnormity analysis
Author
Jinhua Fan ; Jianying Song ; Jie Peng ; Xianfeng Guo
Author_Institution
Taiyuan Satellite Launch Center, Taiyuan, China
fYear
2015
fDate
23-25 May 2015
Firstpage
1812
Lastpage
1816
Abstract
To obtain reasonably the apparent acceleration and angular velocity values from the inertial measurement unit (IMU) telemetry data, a data pre-processing framework is proposed based on abnormity analysis. By introducing some concepts such as continuous/noncontinuous time point (CTP/NCTP), local maximum impulse number, and so on, the abnormity analysis can be implemented according to the characteristics of the IMU output data. Based on the abnormal data positioning results from both the time point sequence and the impulse number sequences, corresponding measures can be taken including the time outlier correction, abnormal parameters correction at CTP, parameters interpolation at NCTP. The IMU telemetry data generated from a missile flight test are used for demonstration, and the effectiveness of the proposed approach is validated.
Keywords
missiles; space telemetry; CTP; IMU telemetry data; NCTP; abnormal data positioning; abnormity analysis; continuous time point; data preprocessing framework; inertial measurement unit; missile flight test; noncontinuous time point; parameter interpolation; time outlier correction; time point sequence; Acceleration; Angular velocity; Filtering; Interpolation; Missiles; Sensors; Telemetry; Abnormity Analysis; Data Pre-Processing; Inertial Measurement Unit;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (CCDC), 2015 27th Chinese
Conference_Location
Qingdao
Print_ISBN
978-1-4799-7016-2
Type
conf
DOI
10.1109/CCDC.2015.7162213
Filename
7162213
Link To Document