首页> 外文期刊>Aircraft Engineering and Aerospace Technology >UAVs and simulation: an experience on MAVs
【24h】

UAVs and simulation: an experience on MAVs

机译:无人机和模拟:MAV的经验

获取原文
获取原文并翻译 | 示例
       

摘要

Purpose - The purpose of this paper is to report the research activity of Politecnico di Torino concerning the MicroHawk platform (micro-aerial vehicles - MAVs) and to present the design and the development of a basic flight simulator for educational/training purpose. Design/methodology/approach - A simulator is an easy-to-use system for the analysis of maneuver response, the dynamic study and the evaluation of the aircraft flying and handling qualities for different aircraft categories. The software implementation, including the definition of mathematical model, the visual scenario and the real-time data analysis graphic interface, are delineated in this paper. In addition to this experimental phase, an important effort is done to incorporate simulation into the autopilot tuning process. Findings - An intense flight activity is carried out to test the flight control system performances of the MicroHawk platform and to establish general procedures to ensure the correct operation of all subsystems. The automatic flight of MAVs has been studied with success for territorial surveillance and map project. Research limitations/implications - In order to simplify the use of these platforms by the end-user, a software interface will be designed to calculate automatically the flight plan, ensuring the desired trajectory design and collision avoidance. Originality/value - The autopilot simulation integrated with vehicle's dynamics can be used to reduce the platform set-up time and the risk of losing the prototype. The simulator training permits to study flight complex plane, in order to obtain better platform performances in real conditions. Starting from a simple scenario, it is possible to set up and upgrade the mission at any time during the simulation.
机译:目的-本文的目的是报告都灵理工大学有关MicroHawk平台(微型航空器-MAV)的研究活动,并介绍用于教育/培训目的的基本飞行模拟器的设计和开发。设计/方法/方法-模拟器是一种易于使用的系统,用于分析机动响应,动态研究以及评估不同类别飞机的飞行和操纵质量。本文描述了软件的实现,包括数学模型的定义,可视化场景和实时数据分析图形界面。除此实验阶段外,还进行了重要的工作,以将仿真合并到自动驾驶仪调整过程中。调查结果-进行了大量的飞行活动,以测试MicroHawk平台的飞行控制系统性能,并建立通用程序以确保所有子系统的正确运行。无人机的自动飞行已经成功地用于领土监视和地图项目的研究。研究局限性/含义-为了简化最终用户对这些平台的使用,将设计一个软件界面来自动计算飞行计划,从而确保所需的轨迹设计和避免碰撞。原创性/价值-与车辆动力学集成的自动驾驶仪仿真可用于减少平台设置时间和丢失原型的风险。仿真器训练允许研究复杂的飞行飞机,以便在实际条件下获得更好的平台性能。从简单的场景开始,可以在仿真过程中随时设置和升级任务。

著录项

  • 来源
    《Aircraft Engineering and Aerospace Technology》 |2009年第1期|p.1-14|共14页
  • 作者单位

    Elisa Capello, Politecnico di Torino, Torino, Italy Giorgio Guglieri, Politecnico di Torino, Torino, Italy Fulvia B. Quagliotti, Politecnico di Torino, Torino, Italy;

  • 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 23:18:25

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号