Modeling Method and Control Strategy for Hose-Drogue Aerial Refueling System

Q4 Engineering
Wu Ling, Sun Yongrong, Huang Bin, Liu Jianye
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引用次数: 1

Abstract

Conventional method for hose-drogue model of aerial refueling system is known to be complex due to the flexible body of hose. And as reported, drogues are unstable in atmospheric turbulence, which greatly decreases docking success rates. This paper proposes a dynamic model for a hose-drogue aerial refueling system based on Kane equation and rigid multi-body dynamics, and analyzes its performance. Furthermore, the nonlinear dynamic model is linearized at the equilibrium point and simplified from full order to 2nd order. Based on the simplified 2nd order model, active control strategies, including proportion integral derivative(PID) and liner quadratic regulator(LQR) control laws, are designed to inhibit the pendulum movement of drogue due to, atmospheric turbulences. Numerical simulation results show the significant correctness of the proposed dynamic model by steady-state drag and balance position of drogue when the tanker flights under different conditions. Moreover, the steady state position error varies within 1 cm, thanks to either controller, when the drogue suffers from moderate-level atmospheric turbulences. Further, the PID controller exhibits better control effect and higher control precision than LQR controller.
软管锥管空中加油系统的建模方法与控制策略
传统的空中加油系统软管-水管模型计算方法由于软管的柔性体而比较复杂。据报道,气流在大气湍流中是不稳定的,这大大降低了对接成功率。基于凯恩方程和刚体多体动力学,提出了软管-喷嘴空中加油系统的动力学模型,并对其性能进行了分析。进一步,将非线性动力学模型在平衡点处线性化,并由全阶简化为二阶。基于简化的二阶模型,设计了比例积分导数(PID)和线性二次调节器(LQR)控制律的主动控制策略,以抑制大气湍流引起的螺旋摆运动。数值仿真结果表明,该模型在不同条件下飞行时的稳态阻力和液滴平衡位置具有显著的正确性。此外,当旋翼遭受中等水平的大气湍流时,由于任一控制器的作用,稳态位置误差在1cm以内。PID控制器比LQR控制器具有更好的控制效果和更高的控制精度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
CiteScore
1.20
自引率
0.00%
发文量
3
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