Design and Experimental Test of Alignment Algorithm based on Inertial Measurement Unit Outputs

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M. Hoseini Saeed; OMIDI HEMMAT OMID; Sabet Mohammad Taghi

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Paper Information

Journal: JOURNAL OF AERONAUTICAL ENGINEERING (JOAE) Year:2018 | Volume:20 | Issue:1 Page(s): 13-24

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Title

Design and Experimental Test of Alignment Algorithm based on Inertial Measurement Unit Outputs

Author(s)

M. Hoseini Saeed | OMIDI HEMMAT OMID | Sabet Mohammad Taghi | Issue Writer Certificate

Keywords

Inertial alignmentQ1

Azimuth angleQ1

Equipping and aimingQ1

Kalman filterQ2

Abstract

In this paper, an alignment algorithm is proposed based on using the outputs of inertial measurement unit (IMU). Accurate initialization of attitude angles containing the Azimuth angle is an important step to increase the accuracy of inertial navigation system output of a moving vehicle. Two step alignment algorithm including course and fine calculation is proposed in this paper which derives the Euler attitude angles including azimuth of vehicle with accuracy of a few arc minutes. First a course alignment is performed based on the components of gravity acceleration and angular velocity of the earth in body coordinate which are measured by inertial measurement unit sensors. Then the fine alignment is performed by constructing an error model of navigation system and estimation of the attitude angles error using a Kalman filter. The observations which are feed to the Kalman filter are the velocity components of vehicle in navigation frame and the eastern angular velocity component of the earth which are zero. To evaluate the accuracy of the proposed alignment algorithm, the IMU is mounted on a 3DOF table which can be aligned with 5 arc second precision as reference attitude. Then the alignment algorithm is executed in several azimuths. The results show the acceptable accuracy of Azimuth angle.

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APA: Copy

M. Hoseini, Saeed, OMIDI HEMMAT, OMID, & Sabet, Mohammad Taghi. (2018). Design and Experimental Test of Alignment Algorithm based on Inertial Measurement Unit Outputs. JOURNAL OF AERONAUTICAL ENGINEERING (JOAE), 20(1 ), 13-24. SID. https://sid.ir/paper/369466/en

Vancouver: Copy

M. Hoseini Saeed, OMIDI HEMMAT OMID, Sabet Mohammad Taghi. Design and Experimental Test of Alignment Algorithm based on Inertial Measurement Unit Outputs. JOURNAL OF AERONAUTICAL ENGINEERING (JOAE)[Internet]. 2018;20(1 ):13-24. Available from: https://sid.ir/paper/369466/en

IEEE: Copy

Saeed M. Hoseini, OMID OMIDI HEMMAT, and Mohammad Taghi Sabet, “Design and Experimental Test of Alignment Algorithm based on Inertial Measurement Unit Outputs,” JOURNAL OF AERONAUTICAL ENGINEERING (JOAE), vol. 20, no. 1 , pp. 13–24, 2018, [Online]. Available: https://sid.ir/paper/369466/en

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