Rigid Body Inertia Estimation Using Extended Kalman and Savitzky-Golay Filters

Inertia properties of rigid body such as ground, aerial, and space vehicles may be changed by several occasions, and this variation of the properties influences the control accuracy of the rigid body. For this reason, accurate inertia properties need to be obtained for precise control. An estimation...

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Main Authors: Donghoon Kim, Sungwook Yang, Sangchul Lee
Format: Article
Language:English
Published: Hindawi Limited 2016-01-01
Series:Mathematical Problems in Engineering
Online Access:http://dx.doi.org/10.1155/2016/2962671
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spelling doaj-4698a03c729649738c16fe10b7eb00052020-11-24T22:27:34ZengHindawi LimitedMathematical Problems in Engineering1024-123X1563-51472016-01-01201610.1155/2016/29626712962671Rigid Body Inertia Estimation Using Extended Kalman and Savitzky-Golay FiltersDonghoon Kim0Sungwook Yang1Sangchul Lee2LG Electronics, Seoul 08592, Republic of KoreaKorea Aerospace University, Goyang 10540, Republic of KoreaKorea Aerospace University, Goyang 10540, Republic of KoreaInertia properties of rigid body such as ground, aerial, and space vehicles may be changed by several occasions, and this variation of the properties influences the control accuracy of the rigid body. For this reason, accurate inertia properties need to be obtained for precise control. An estimation process is required for both noisy gyro measurements and the time derivative of the gyro measurements. In this paper, an estimation method is proposed for having reliable estimates of inertia properties. First, the Euler equations of motion are reformulated to obtain a regressor matrix. Next, the extended Kalman filter is adopted to reduce the noise effects in gyro angular velocity measurements. Last, the inertia properties are estimated using linear least squares. To achieve reliable and accurate angular accelerations, a Savitzky-Golay filter based on an even number sampled data is utilized. Numerical examples are presented to demonstrate the performance of the proposed algorithm for the case of a space vehicle. The numerical simulation results show that the proposed algorithm provides accurate inertia property estimates in the presence of noisy measurements.http://dx.doi.org/10.1155/2016/2962671
collection DOAJ
language English
format Article
sources DOAJ
author Donghoon Kim
Sungwook Yang
Sangchul Lee
spellingShingle Donghoon Kim
Sungwook Yang
Sangchul Lee
Rigid Body Inertia Estimation Using Extended Kalman and Savitzky-Golay Filters
Mathematical Problems in Engineering
author_facet Donghoon Kim
Sungwook Yang
Sangchul Lee
author_sort Donghoon Kim
title Rigid Body Inertia Estimation Using Extended Kalman and Savitzky-Golay Filters
title_short Rigid Body Inertia Estimation Using Extended Kalman and Savitzky-Golay Filters
title_full Rigid Body Inertia Estimation Using Extended Kalman and Savitzky-Golay Filters
title_fullStr Rigid Body Inertia Estimation Using Extended Kalman and Savitzky-Golay Filters
title_full_unstemmed Rigid Body Inertia Estimation Using Extended Kalman and Savitzky-Golay Filters
title_sort rigid body inertia estimation using extended kalman and savitzky-golay filters
publisher Hindawi Limited
series Mathematical Problems in Engineering
issn 1024-123X
1563-5147
publishDate 2016-01-01
description Inertia properties of rigid body such as ground, aerial, and space vehicles may be changed by several occasions, and this variation of the properties influences the control accuracy of the rigid body. For this reason, accurate inertia properties need to be obtained for precise control. An estimation process is required for both noisy gyro measurements and the time derivative of the gyro measurements. In this paper, an estimation method is proposed for having reliable estimates of inertia properties. First, the Euler equations of motion are reformulated to obtain a regressor matrix. Next, the extended Kalman filter is adopted to reduce the noise effects in gyro angular velocity measurements. Last, the inertia properties are estimated using linear least squares. To achieve reliable and accurate angular accelerations, a Savitzky-Golay filter based on an even number sampled data is utilized. Numerical examples are presented to demonstrate the performance of the proposed algorithm for the case of a space vehicle. The numerical simulation results show that the proposed algorithm provides accurate inertia property estimates in the presence of noisy measurements.
url http://dx.doi.org/10.1155/2016/2962671
work_keys_str_mv AT donghoonkim rigidbodyinertiaestimationusingextendedkalmanandsavitzkygolayfilters
AT sungwookyang rigidbodyinertiaestimationusingextendedkalmanandsavitzkygolayfilters
AT sangchullee rigidbodyinertiaestimationusingextendedkalmanandsavitzkygolayfilters
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