In-Flight Estimation of Center of Gravity Position Using All-Accelerometers

Changing the position of the Center of Gravity (CoG) for an aerial vehicle is a challenging part in navigation, and control of such vehicles. In this paper, an all-accelerometers-based inertial measurement unit is presented, with a proposed method for on-line estimation of the position of the CoG....

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Main Authors: Yazan Mohammad Al-Rawashdeh, Moustafa Elshafei, Mohammad Fahad Al-Malki
Format: Article
Language:English
Published: MDPI AG 2014-09-01
Series:Sensors
Subjects:
Online Access:http://www.mdpi.com/1424-8220/14/9/17567
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author Yazan Mohammad Al-Rawashdeh
Moustafa Elshafei
Mohammad Fahad Al-Malki
author_facet Yazan Mohammad Al-Rawashdeh
Moustafa Elshafei
Mohammad Fahad Al-Malki
author_sort Yazan Mohammad Al-Rawashdeh
collection DOAJ
description Changing the position of the Center of Gravity (CoG) for an aerial vehicle is a challenging part in navigation, and control of such vehicles. In this paper, an all-accelerometers-based inertial measurement unit is presented, with a proposed method for on-line estimation of the position of the CoG. The accelerometers’ readings are used to find and correct the vehicle’s angular velocity and acceleration using an Extended Kalman Filter. Next, the accelerometers’ readings along with the estimated angular velocity and acceleration are used in an identification scheme to estimate the position of the CoG and the vehicle’s linear acceleration. The estimated position of the CoG and motion measurements can then be used to update the control rules to achieve better trim conditions for the air vehicle.
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spelling doaj.art-90bd67660022489892134a44a7ec02402022-12-22T02:06:32ZengMDPI AGSensors1424-82202014-09-01149175671758510.3390/s140917567s140917567In-Flight Estimation of Center of Gravity Position Using All-AccelerometersYazan Mohammad Al-Rawashdeh0Moustafa Elshafei1Mohammad Fahad Al-Malki2Department of Systems Engineering, King Fahd University of Petroleum and Minerals, Dhahran 31261, Saudi ArabiaDepartment of Systems Engineering, King Fahd University of Petroleum and Minerals, Dhahran 31261, Saudi ArabiaTechnical & Industrial Services Co., Dammam 31493, Saudi ArabiaChanging the position of the Center of Gravity (CoG) for an aerial vehicle is a challenging part in navigation, and control of such vehicles. In this paper, an all-accelerometers-based inertial measurement unit is presented, with a proposed method for on-line estimation of the position of the CoG. The accelerometers’ readings are used to find and correct the vehicle’s angular velocity and acceleration using an Extended Kalman Filter. Next, the accelerometers’ readings along with the estimated angular velocity and acceleration are used in an identification scheme to estimate the position of the CoG and the vehicle’s linear acceleration. The estimated position of the CoG and motion measurements can then be used to update the control rules to achieve better trim conditions for the air vehicle.http://www.mdpi.com/1424-8220/14/9/17567in-flightcenter of gravity determinationall-accelerometersIMU
spellingShingle Yazan Mohammad Al-Rawashdeh
Moustafa Elshafei
Mohammad Fahad Al-Malki
In-Flight Estimation of Center of Gravity Position Using All-Accelerometers
Sensors
in-flight
center of gravity determination
all-accelerometers
IMU
title In-Flight Estimation of Center of Gravity Position Using All-Accelerometers
title_full In-Flight Estimation of Center of Gravity Position Using All-Accelerometers
title_fullStr In-Flight Estimation of Center of Gravity Position Using All-Accelerometers
title_full_unstemmed In-Flight Estimation of Center of Gravity Position Using All-Accelerometers
title_short In-Flight Estimation of Center of Gravity Position Using All-Accelerometers
title_sort in flight estimation of center of gravity position using all accelerometers
topic in-flight
center of gravity determination
all-accelerometers
IMU
url http://www.mdpi.com/1424-8220/14/9/17567
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AT moustafaelshafei inflightestimationofcenterofgravitypositionusingallaccelerometers
AT mohammadfahadalmalki inflightestimationofcenterofgravitypositionusingallaccelerometers