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首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers >Soft landing control of unmanned powered parafoils in unknown wind environments
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Soft landing control of unmanned powered parafoils in unknown wind environments

机译:未知风环境下无人动力翼型飞机的软着陆控制

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摘要

For autonomous landing powered parafoils, the ability to perform a final flare maneuver against the wind direction can generate a considerable reduction of lateral and longitudinal velocities at impact, enabling a soft landing for a safe delivery of sensible loads. To realize accurate, soft landing in the unknown wind environment, an in-flight wind identification algorithm is first proposed. The wind direction and speed can be obtained online by only using the GPS sampling data based on the recursive least square method. Moreover, the 3D trajectory tracking strategy for the powered parafoil is also established, which is globally asymptotically stable. Furthermore, the lateral trajectory tracking controller and longitudinal altitude controller based on active disturbance rejection control are presented, respectively. Eventually, results from simulations demonstrate that the proposed landing control method can effectively realize accurate soft landing in unknown wind environments with the in-flight wind identification algorithm applied in the trajectory tracking process.
机译:对于自主着陆动力翼型,逆风方向执行最终火炬机动的能力会大大降低撞击时的横向和纵向速度,从而实现软着陆,以安全地输送合理的载荷。为了在未知风环境下实现精确的软着陆,首先提出了一种飞行中风识别算法。仅可以使用基于递归最小二乘法的GPS采样数据在线获取风向和风速。此外,还建立了动力翼型飞机的3D轨迹跟踪策略,该策略在全局上是渐近稳定的。此外,分别提出了基于主动扰动抑制控制的横向轨迹跟踪控制器和纵向高度控制器。最终,仿真结果表明,所提出的着陆控制方法可以通过在轨迹跟踪过程中应用飞行中风识别算法,在未知风环境下有效实现精确的软着陆。

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