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Fast trajectory planning based on in-flight waypoints for unmanned aerial vehicles

机译:基于飞行中航路点的无人飞行器快速轨迹规划

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摘要

Purpose - The purpose of this paper is to propose an efficient algorithm for trajectory planning of unmanned aerial vehicles (UAVs) in 2D spaces. This paper has been motivated by the challenge to develop a fast trajectory planning algorithm for autonomous UAVs through mid-course waypoints (WPs). It is assumed that there is no prior knowledge of these WPs, and their configuration is computed as in-flight procedure. Design/methodology/approach - Since the off-line techniques cannot be applied, it is required to apply an online trajectory planning algorithm. For this reason, based on the optimal control and the geometry, each segment of trajectory is designed with respect to a local frame. The algorithm is implemented as a real-time manner in terms of the down-range variable. Findings - The proposed algorithm tries to find not only a feasible trajectory (the constraint includes the maximum heading angle rate) but also an optimal trajectory (the objective locally is to minimize the length of the path). This online trajectory planning algorithm gradually produces a smooth 2D trajectory aiming at reaching the mid-course WPs and the final target so that they are smoothly connected with each other. The mid-course WPs are described through the given down-range, cross-range, and heading angle. Originality/value - Based on geometrical principles, this algorithm is capable of re-planning the trajectory as in-flight manner, and the computational burden approaches the online capabilities for UAVs with high velocity.
机译:目的-本文的目的是提出一种有效的2D空间无人飞行器(UAV)轨迹规划算法。受到挑战的启发,本文为通过中途航路点(WP)开发用于自主无人机的快速轨迹规划算法。假定没有这些WP的先验知识,并且它们的配置是在飞行过程中计算的。设计/方法/方法-由于无法应用离线技术,因此需要应用在线轨迹规划算法。因此,基于最佳控制和几何形状,相对于局部框架设计轨迹的每个部分。根据下限变量,该算法以实时方式实现。结果-提出的算法不仅试图找到可行的轨迹(约束条件包括最大航向角速率),而且还寻求最优轨迹(局部目标是使路径长度最小化)。该在线轨迹规划算法逐渐生成平滑的2D轨迹,旨在达到路线中间WP和最终目标,从而使它们彼此平滑连接。通过给定的下范围,跨范围和航向角来描述路线中段WP。独创性/价值-基于几何原理,该算法能够以飞行方式重新规划轨迹,并且计算负担接近高速无人机的在线功能。

著录项

  • 来源
    《Aircraft Engineering and Aerospace Technology》 |2010年第2期|p.1-10|共10页
  • 作者

    A.R. Babaei M. Mortazavi;

  • 作者单位

    A.R. Babaei, Aerospace Engineering Department, Amirkabir University of Technology, Tehran, Iran M. Mortazavi, Aerospace Engineering Department, Center of Excellence in Computational Aerospace, Amirkabir University of Technology, Tehran, Iran;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 23:18:14

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