系统仿真学报 ›› 2016, Vol. 28 ›› Issue (1): 220-226.

• 仿真应用工程 • 上一篇    下一篇

无人机无动力返场航迹规划与控制仿真

张毅君1, 董一群1, 詹光2, 艾剑良1   

  1. 1.复旦大学力学与工程科学系复旦大学飞行器设计研究所, 上海 200433;
    2.沈阳飞机设计研究所,沈阳 110035
  • 收稿日期:2014-09-01 修回日期:2015-03-17 发布日期:2020-07-02
  • 作者简介:张毅君(1989-),男,上海,硕士,研究方向为飞行力学与飞行控制;董一群(1990-),男,宿迁,博士,研究方向为飞行力学与飞行控制;詹光(1980-),男,沈阳,硕士,高工,研究方向为飞行器设计。

Path Planning and Control Simulation of Unpowered Unmanned Aerial Vehicle (UAV) Returning to The Airport

Zhang Yijun1, Dong Yiqun1, Zhan Guang2, Ai Jianliang1   

  1. 1. Institute of Aircraft Design, Department of Mechanics and engineering science, Fudan University, Shanghai 200433, China;
    2. Institute of Shenyang Aircraft Design, Shenyang 110035, China
  • Received:2014-09-01 Revised:2015-03-17 Published:2020-07-02

摘要: 无人机无动力返场是飞行过程中风险巨大、技术复杂的环节,是影响无人机飞行安全的关键阶段。从无人机滑翔过程中的能量变化出发,研究无人机无动力返场飞行的基本控制策略及返场航迹规划,提出了返程平均阻力的计算方法。在无障碍条件下,建立了返程着陆飞行控制规律模型。仿真结果表明方法行之有效,为下一步无人机无动力在规定区域安全着陆的边界包线的计算奠定了基础。

关键词: 无人机, 无动力返场, 控制策略, 航迹规划, 返场平均阻力

Abstract: The unpowered Unmanned Aerial Vehicle (UAV) return to the airport unpoweredly is a link of large risk and complex technology during the flight, and it is the key stage which affects the flight safety of the UAV. The basic control strategy and path planning of the unpowered UAV's back to the airport were studied, and the method which calculated the average drag of the return was proposed. Under the condition of multiple constraints, the flight control model of the UAV's return was established. It is proved that the result of the simulation is effective and has built a foundation for the calculation of the boundary envelope which the unpowered UAV can safely land in the designated areas.

Key words: UAV, back to the airport unpoweredly, control strategy, flight path planning, average drag of the return

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