Abstract

In this paper, we summarize the results of using dynamic models borrowed from tracking theory in describing the time evolution of the state vector to have an estimate of the angular motion in a gyro-free inertial measurement unit (GF-IMU). The GF-IMU is a special type inertial measurement unit (IMU) that uses only a set of accelerometers in inferring the angular motion. Using distributed accelerometers, we get an angular information vector (AIV) composed of angular acceleration and quadratic angular velocity terms. We use a Kalman filter approach to estimate the angular velocity vector since it is not expressed explicitly within the AIV. The bias parameters inherent in the accelerometers measurements' produce a biased AIV and hence the AIV bias parameters are estimated within an augmented state vector. Using dynamic models, the appended bias parameters of the AIV become observable and hence we can have unbiased angular motion estimate. Moreover, a good model is required to extract the maximum amount of information from the observation. Observability analysis is done to determine the conditions for having an observable state space model. For higher grades of accelerometers and under relatively higher sampling frequency, the error of accelerometer measurements is dominated by the noise error. Consequently, simulations are conducted on two models, one has bias parameters appended in the state space model and the other is a reduced model without bias parameters.

Highlights

  • A conventional inertial measurement unit (IMU) is composed of three accelerometers and three gyroscopes mounted in a strap-down configuration

  • The rest of this paper is organized as follows: Section 2 gives a background about the angular motion estimation in a gyro-free inertial measurement unit (GF-IMU) and describes the configuration used in this work

  • Three-dimensional harmonic angular oscillation is considered as a coning motion, the GF-IMU system responds better in this case because of having all the angular information vector (AIV) terms as non-zero, which increases observability

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Summary

Introduction

A conventional IMU is composed of three accelerometers and three gyroscopes mounted in a strap-down configuration. The bias instability is the dominant error because the inertial system often works as a standalone system. Inertial systems can be categorized in terms of gyro bias error [1]. The use of distributed accelerometers as an alternative to conventional gyros to infer the angular motion has been a subject of intensive research. Unlike the standard IMU, the GF-IMU uses only accelerometers to infer the acceleration and the angular velocity. The rest of this paper is organized as follows: Section 2 gives a background about the angular motion estimation in a GF-IMU and describes the configuration used in this work.

Angular Motion Estimation in a GF-IMU
GF-IMU Fixed Accelerometers Configurations
Dynamic Models to Be Considered
Wiener-Process Angular Acceleration Model
Other Models to Be Considered
The Accelerometer Error Model
The Measured AIV
Calibration and Initial Bias Estimation in a GF-IMU
An EKF Solution Using the Singer Model with Appended Bias Parameters
Prediction
Measurement Update
Observability Analysis
An EKF Solution Using the Singer Model without Appending Bias Parameters
Simulation Results for the Augmented Model
Trajectory Profile and Parameters Setting
Results and Analysis
Effect of Improper Initialization
Simulation Results for Non-Augmented Model
Trajectory Profile and Parameter Setting
Conclusions

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