Robust 3-D low-altitude airdrop flight control via the sigmoid function-based observer

Zikang Su, Zunkun Cheng, Honglun Wang
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Abstract

A robust 3-D trajectory tracking controller for the low-altitude airdrop of the transport aircraft is established in the presence of airflow disturbances, by combining the back- stepping technique and sigmoid function-based disturbance observer. The transport aircraft’s nonlinear dynamics during the low-altitude airdrop process is modeled in the affine nonlinear form which consists of the effect of the movement and abrupt drop of the heavy cargo, the ground effect, and the airflow disturbances. The three-dimensional airdrop flight controller design is divided into several cascade subsystems, via the back-stepping technique. In each subsystem dynamic, items caused by the disturbances during the extraction are viewed as part of the "lumped disturbances". They are individually reconstituted and compensated via the sigmoid function-based disturbance observers with high estimation accuracy and nice disturbance attenuation ability. With the estimated the lumped disturbances, an anti-disturbance 3-D back-stepping based controller is proposed for the low-altitude airdrop. Simulations are carried out to verify the proposed control method’s effectiveness in improving the robustness and tracking accuracy.
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基于s型函数观测器的三维低空空投飞行控制
结合基于s型函数的扰动观测器和后退技术,建立了存在气流扰动的运输机低空空投的鲁棒三维轨迹跟踪控制器。将运输机低空空投过程中的非线性动力学建模为仿射非线性模型,该模型考虑了重型货物的运动和突降、地面效应和气流扰动的影响。将三维空投飞行控制器设计分为若干级联子系统,采用退步技术。在每个动态子系统中,提取过程中由扰动引起的项被视为“集总扰动”的一部分。它们通过基于s型函数的干扰观测器分别重构和补偿,具有较高的估计精度和良好的干扰衰减能力。在估计了集总扰动的基础上,提出了一种基于三维反演的低空空投抗干扰控制器。通过仿真验证了所提控制方法在提高鲁棒性和跟踪精度方面的有效性。
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