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ON SAFETY ASSESSEMENT OF NOVEL APPROACH TO ROBUST UAV FLIGHT CONTROL IN GUSTY ENVIRONMENTS

机译:尘环境下鲁棒无人机飞行控制新方法的安全性评估

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In a follow-up to our previous study [1], thecurrent work examines the gust-induced “coneof uncertainty” in a small unmanned aerialvehicle’s (UAV) flight trajectory addressed inthe context of safety assessments of UAVoperations. Such analysis is a critical facet ofthe integration of unmanned aerial systems(UAS) into the National Airspace System (NAS),particularly in terminal airspace. The paperdescribes a predictive, robust feedback-loopflight control model that is applicable to variousclasses of UAVs and unsteady flight-pathscenarios. The control design presented in thispaper extends previous research results bydemonstrating asymptotic (zero steady-stateerror) altitude regulation control in thepresence of unmodeled vertical wind gustdisturbances. To address the practicalconsiderations involved in small UAVapplications with limited computationalresources, the proposed control method isdesigned with a computationally simplisticstructure, without the requirement of complexcalculations or function approximators in thecontrol loop. Proof of the theoretical result issummarized, and detailed numerical simulationresults are provided, which demonstrate thecapability of the proposed nonlinear controlmethod to asymptotically reject wind gustdisturbances and parameter variations in thestate space model. Simulation comparisons witha standard linear control method are providedfor completeness.
机译:在我们之前的研究[1]的后续研究中, 当前的工作是检查阵风引起的“锥体” 小型无人驾驶飞机的不确定性” 的(UAV)飞行轨迹 无人机安全评估的背景 操作。这种分析是 无人机系统的整合 (UAS)进入国家空域系统(NAS), 特别是在终端空域。论文 描述了一个预测性的,健壮的反馈回路 适用于各种飞行控制模型 无人机的类别和不稳定的飞行路径 场景。本节介绍的控制设计 该论文通过以下方式扩展了先前的研究结果 展示渐近(零稳态 错误)中的高度调节控制 存在未建模的垂直阵风 干扰。解决实际 小型无人机涉及的注意事项 计算量有限的应用程序 资源,建议的控制方法是 设计简单 结构,无需复杂 中的计算或函数逼近器 控制回路。理论结果的证明是 总结和详细的数值模拟 提供的结果表明了 非线性控制的能力 渐近拒绝阵风的方法 干扰和参数变化 状态空间模型。仿真比较 提供了标准的线性控制方法 为了完整性。

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