Abstract

In the motion control of AUVs, especially those driven by multiple thrusters, the thruster misalignment and thrust loss cause the actual force and moment applied to the AUV to deviate from that desired, making accurate and fast motion control difficult. This paper proposes a sliding mode control method with dual-observer estimation for the AUV 3D motion control problem in the presence of thruster misalignment uncertainty and thrust loss uncertainty. Firstly, this paper considers the force and moment deviation as disturbances that vary with the controller output, and proposes the TD disturbance observer to address the problem of deviation caused by uncertainty in thruster misalignment. Secondly, this paper introduces the dynamics equation of thrust loss and designs the gain disturbance observer to estimate the thrust loss uncertainty during AUV navigation. The designed controller, verified by simulation and field tests, ensures that the AUV maintains better motion control despite thruster misalignment and thrust loss.

Highlights

  • IntroductionAUV has been an active field of research and development in exploring unknown marine environments and carrying out different military missions [1]

  • This paper proposes a disturbance observer based on a tracking differentiator for AUV motion control with the uncertainty of thruster misalignment

  • This paper introduces the thruster dynamics model and proposes the gain oretically proves the convergence of the gain disturbance observer

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Summary

Introduction

AUV has been an active field of research and development in exploring unknown marine environments and carrying out different military missions [1]. The main contributions of this paper are as follows: Firstly, this paper proposes a disturbance observer based on a tracking differentiator for AUV motion control with the uncertainty of thruster misalignment. This paper introduces the thruster dynamics model gain and moment deviations are regarded as disturbances with and the proposes change ofthe control ance observer, and the stability of the controller and convergence of the TD disturbdisturbance observer to estimate themode uncertainty thrusteristhrust loss.

Problem
Controller Design
ΔF3 loss
Simulation Test
10. Vertical
16. Vertical
Field Test
26. Velocity
35. Thruster
Conclusions
Full Text
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