Abstract

In this paper, the autonomous landing control issue on moving shipboard is investigated for unmanned helicopters subject to disturbances. The issue is studied by stabilizing the error system of the helicopter and the shipboard. The landing process is divided into two phases, i.e., homing phase, where a hierarchical double-loop control scheme is developed such that the helicopter is forced to hover synchronously at a certain altitude over the shipboard, and landing phase, where a composite landing control scheme is proposed such that the helicopter lands vertically on the shipboard in synchronization with its attitudes. The velocity and acceleration information of the shipboard as well as lump disturbances is estimated through joint state and disturbance observers. The estimates are then incorporated into the baseline feedback controller, formulating composite active anti-disturbance landing control schemes. A continuous terminal sliding mode control method is proposed for the feedback controller design, which not only effectively mitigates the chattering of the control action, but also simplifies the design process of the controller. Numerical simulations demonstrate the effectiveness and superiorities of the proposed control schemes.

Highlights

  • Unmanned aerial vehicles (UAVs) have received a great deal of research, development and application for several decades [1]

  • The autonomous landing control problem on moving shipboard has been investigated for disturbed helicopters in this paper

  • By dividing the whole landing process into homing phase and landing phase, the helicopter has been forced to land on a moving shipboard from a distant location

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Summary

Introduction

Unmanned aerial vehicles (UAVs) have received a great deal of research, development and application for several decades [1]. In all operating environments, maritime operating is very precarious and challenging due to the rough sea conditions such as low visibility, strong wind and turbulence, unpredictable motions of the shipboard, and narrow deck space [1]. For these two reasons, it is of great academic significance and research value to exploit autonomous landing schemes for helicopters on moving shipboard. Many researches have been carried out on autonomous landing of UAVs on moving targets. Many nonlinear control methods have been proposed, such as robust H∞ control [10, 11], backstepping control [12, 13], and sliding mode control (SMC) [14,15,16]

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