Co-Regulation of Computational and Physical Effectors in a Quadrotor Unmanned Aircraft System

Xinkai Zhang, Seth Doebbeling, Justin M. Bradley
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引用次数: 4

Abstract

Traditional control strategies rely on real-time computer tasks executing in fixed intervals providing periodic sampling upon which discrete controllers are designed. But emerging trends challenge this fixed resource allocation strategy by sampling at the "right" time rather than at fixed intervals. We propose a strategy in which a model representing the sampling rate is augmented to the state-space model of a quadrotor unmanned aircraft system, coupled controllers are designed for this holistic system, and computational and physical effectors are co-regulated in response to system performance. We investigate a new discrete-time-varying control strategy by gain scheduling a discrete linear quadratic regulator controller at a series of sampling rates, and co-regulating the sampling rates using a cyber controller whose gains are optimized via a strategic cost function. We then show step responses of the quadrotor to demonstrate how rapid changes in physical system gain at discrete sampling rates negatively impacts system performance. To solve this we introduce a new cyber control strategy that reduces these negative impacts and show how the response can be improved. Since most multicopters employ waypoint tracking planning and guidance, we also evaluate our strategy by assessing performance of the quadrotor in following a waypoint trajectory giving a much better indication of how a control strategy affects mission performance. We develop cyber-physical metrics for assessing waypoint following performance and use them to improve controller design. Results show that our proposed coupled cyber-physical system model and controller can provide physical system performance similar to fixed-rate optimal control strategies but with less control effort and much less computational utilization. Our strategy allows cyber and physical resources to be dynamically allocated to system demands as needed.
四旋翼无人机系统中计算效应器和物理效应器的协同调节
传统的控制策略依赖于以固定间隔执行的实时计算机任务,并提供周期性采样,在此基础上设计离散控制器。但是,新兴趋势通过在“正确”的时间而不是固定的间隔取样,挑战了这种固定的资源分配策略。我们提出了一种策略,该策略将表示采样率的模型扩展到四旋翼无人机系统的状态空间模型中,为该整体系统设计耦合控制器,并根据系统性能共同调节计算和物理效应器。我们研究了一种新的离散时变控制策略,该策略是在一系列采样率下调度一个离散线性二次型调节器控制器的增益,并使用一个通过策略成本函数优化增益的网络控制器来共同调节采样率。然后,我们展示了四旋翼的阶跃响应,以证明在离散采样率下物理系统增益的快速变化如何对系统性能产生负面影响。为了解决这个问题,我们引入了一种新的网络控制策略,可以减少这些负面影响,并展示如何改进响应。由于大多数多旋翼机采用航路点跟踪规划和指导,我们也通过评估四旋翼机在航路点轨迹下的性能来评估我们的策略,从而更好地说明控制策略如何影响任务性能。我们开发了用于评估航路点跟踪性能的网络物理指标,并使用它们来改进控制器设计。结果表明,我们提出的耦合网络-物理系统模型和控制器可以提供与固定速率最优控制策略相似的物理系统性能,但控制工作量更少,计算利用率更低。我们的策略允许网络和物理资源根据需要动态分配给系统需求。
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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