无人机攻击机动:一种数据知情的无模型方法

IF 3.2 3区 计算机科学 Q2 AUTOMATION & CONTROL SYSTEMS
Cong Li, Xinglong Zhang, Xin Xu, Yong Wang, Xiangke Wang
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引用次数: 0

摘要

无人驾驶飞行器(uav)有望充分利用其机动能力,在恶劣环境下完成竞速和特技飞行等任务。然而,大多数相关的工作往往集中在缓慢的动作上,只适合在结构良好的环境中进行常规任务。这促使我们提出一种高度鲁棒的控制方案,专门为无人机侵略性机动设计,通过快速和大的位置或姿态变化进行编码。我们的方法的核心是数据知情的增量动力学和四元数促进控制方案。前者有利于无模型控制,消除了在高速和加速度下精确建模复杂动力学的要求;而后者在大角度变化时避免了潜在的奇点。特别是,我们首先利用一步向后的数据来构建增量动力学,这是无人机动力学的无模型表示。然后,将构建的增量动力学作为位置优先和姿态优先控制方案发展的基础,设计了基于四元数的主动机动跟踪控制器,并进行了完整的理论分析。选择三/四/六/八旋翼平台的轮盘、桶滚、多重翻转和眼镜蛇等侵略性机动,对我们提出的位置优先和姿态优先控制方案的性能进行了评估,其中线速度高达20 m/s $$ 20\kern0.3em \mathrm{m}/\mathrm{s} $$。角度变化可达360°$$ {360}^{{}^{\circ}} $$。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Aggressive Maneuver for Unmanned Aerial Vehicle: A Data-Informed Model Free Method

Unmanned aerial vehicles (UAVs) are expected to fully exploit their maneuvering capabilities to conduct aggressive maneuvers to complete tasks such as racing and aerobatics even in harsh environments. However, most of the related works often focus on slow movements only suitable for regular tasks in well-structured environments. This motivates us to propose a highly robust control scheme designed specifically for UAV aggressive maneuvers, encoded by rapid and large changes in either position or attitude. The core of our approach is the data-informed incremental dynamics and the quaternion facilitated control scheme. The former facilitates the model-free control that eliminates the requirement to model the complex dynamics at high velocities and accelerations accurately; While the latter avoids potential singularities during large angular changes. In particular, we first utilize one-step-backward data to construct incremental dynamics, a model-free representation of the UAV dynamics. Then, the constructed incremental dynamics serves as the basis for the development of both position-priority and attitude-priority control schemes, wherein the novel quaternion based aggressive maneuver tracking controllers are designed with complete theoretical analysis. The aggressive maneuvers such as roulette, barrel roll, multiple-flip and cobra maneuvers are chosen for tri/quad/hexa/octocopter platforms to evaluate the performance of our proposed position-priority and attitude-priority control schemes, during which the linear velocity up to 20 m/s $$ 20\kern0.3em \mathrm{m}/\mathrm{s} $$ , the angular changes up to 360 ° $$ {360}^{{}^{\circ}} $$ .

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来源期刊
International Journal of Robust and Nonlinear Control
International Journal of Robust and Nonlinear Control 工程技术-工程:电子与电气
CiteScore
6.70
自引率
20.50%
发文量
505
审稿时长
2.7 months
期刊介绍: Papers that do not include an element of robust or nonlinear control and estimation theory will not be considered by the journal, and all papers will be expected to include significant novel content. The focus of the journal is on model based control design approaches rather than heuristic or rule based methods. Papers on neural networks will have to be of exceptional novelty to be considered for the journal.
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