2016
DOI: 10.1088/0957-0233/27/7/075105
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Improved calibration of IMU biases in analytic coarse alignment for AHRS

Abstract: An improved method for the inertial measurement unit (IMU) calibration of coarse alignment for the low-accuracy attitude heading reference system (AHRS) is proposed in this paper. The sensitivities of the Euler angles with respect to the inertial sensor biases are studied based on the analytic coarse alignment principle, and the errors of earth rotation rate and local gravity in the body frame caused by initial attitude error are analyzed. Then, an improved analytic coarse alignment algorithm with acceleromete… Show more

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Cited by 14 publications
(10 citation statements)
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“…Several literatures have elaborated on the steps taken to handle the occurrences of drifts in its output. Amongst such are as reported in [21], [22], [23] that introduces the application of Attitude and Heading Reference System (AHRS) sensor fusion algorithm which utilizes the Quaternion estimation such as to filter out the aforementioned drift effect [24], [25]. This is done by rotating the body frame vector into inertial frame vector using the rotation matrix defined as:…”
Section: Hardware Descriptionmentioning
confidence: 99%
“…Several literatures have elaborated on the steps taken to handle the occurrences of drifts in its output. Amongst such are as reported in [21], [22], [23] that introduces the application of Attitude and Heading Reference System (AHRS) sensor fusion algorithm which utilizes the Quaternion estimation such as to filter out the aforementioned drift effect [24], [25]. This is done by rotating the body frame vector into inertial frame vector using the rotation matrix defined as:…”
Section: Hardware Descriptionmentioning
confidence: 99%
“…The performance of SINS depends on the accuracy and rapidity of the initial alignment process, which can be divided into coarse alignment and fine alignment [5,6]. Coarse alignment is important since it provides a rapidly alignment result for the fine alignment.…”
Section: Introductionmentioning
confidence: 99%
“…SINS is widely used in aviation, marine, land vehicle navigation and positioning because of its advantage of complete autonomy [ 3 , 4 ]. The SINS capability depends on the accuracy and rapidity of initial alignment process which is one of the key technologies in SINS [ 5 , 6 ]. The research about static base initial alignment has been done very well [ 7 , 8 ], however, how to complete the initial alignment of the inertial navigation system on moving base becomes an urgent problem to be solved.…”
Section: Introductionmentioning
confidence: 99%