Abstract

The solution of the dynamic equations of the six-axis accelerometer is a prerequisite for sensor calibration, structural optimization, and practical application. However, the forward dynamic equations (FDEs) and inverse dynamic equations (IDEs) of this type of system have not been completely solved due to the strongly nonlinear coupling relationship between the inputs and outputs. This article presents a comprehensive study of the FDEs and IDEs of the six-axis accelerometer based on a parallel mechanism. Firstly, two sets of dynamic equations of the sensor are constructed based on the Newton–Euler method in the configuration space. Secondly, based on the analytical solution of the sensor branch chain length, the coordination equation between the output signals of the branch chain is constructed. The FDEs of the sensor are established by combining the coordination equations and two sets of dynamic equations. Furthermore, by introducing generalized momentum and Hamiltonian function and using Legendre transformation, the vibration differential equations (VDEs) of the sensor are derived. The VDEs and Newton–Euler equations constitute the IDEs of the system. Finally, the explicit recursive algorithm for solving the quaternion in the equation is given in the phase space. Then the IDEs are solved by substituting the quaternion into the dynamic equations in the configuration space. The predicted numerical results of the established FDEs and IDEs are verified by comparing with virtual and actual experimental data. The actual experiment shows that the relative errors of the FDEs and the IDEs constructed in this article are 2.21% and 7.65%, respectively. This research provides a new strategy for further improving the practicability of the six-axis accelerometer.

Highlights

  • The robustness of the control system can be improved by introducing acceleration feedback in the robot control system [1]

  • Both the inertial measurement units (IMUs) and the six-axis accelerometer are used to measure the vibration of the vibration shaker, and the IMU measurement results are regarded as standard values

  • The results of the virtual and actual experiments demonstrate the accuracy of the dynamic model and the practicability of the six-axis accelerometer proposed in this article

Read more

Summary

Introduction

The robustness of the control system can be improved by introducing acceleration feedback in the robot control system [1]. Inspired by the design scheme of the six-axis force sensor based on the Stewart platform, some scholars proposed and studied the six-axis acceleration measurement scheme that only contained one inertial unit by using the Stewart platform as the elastic body of the sensor [26,27,28,29,30]. Xia et al [30] proposed a method for modeling the IDEs of a six-axis accelerometer based on the Kane’s dynamics equation This scheme introduces more kinematics items, which leads to the real-time performance of the algorithm cannot be guaranteed. On the other hand, based on the Newton–Euler equation and Hamiltonian equation, the IDEs of the sensor are analyzed, and the solution process of the IDEs that can realize the real-time decoupling of the measured acceleration is given.

Structural Design
Prototype of the accelerometer:
The exploded3-D
Principle model coordinate system:
Dynamic Analysis of the System
Forward Dynamics
Equation Establishment
Equation Solving
Actual
Inertial
Actual Experiment 1
Actual Experiment 2
Findings
Conclusions and Discussion
Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call