小型无人机的伞降回收轨迹研究  

Research on Parachute Landing Track for Mini UAVS

作　　者：王天雨[1] 赵鑫宇[1] 薛东彬[1] 

机构地区：[1]中国电子科技集团公司第二十七研究所,郑州450047

出　　处：《电光系统》2009年第4期49-54,共6页Electronic and Electro-optical Systems

摘　　要：本文针对小型无人机伞降回收特点，设计了用于该系统的定点回收系统。该系统充分考虑工程约束，建立了基于风场扰动的回收模型，通过分析飞机回收阶段的受力，建立了无人机伞降运动模型，规划了回收段航迹，并进行了仿真分析。结果表明，系统能够满足要求，得到回收轨迹。Focused on the characteristics of parachute landing of mini unmanned aerial vehicle （ UAV）, a point- ing recovery system for UAV landing was designed. Considering the engineering restriction, a landing model based on wind disturbance was established. By analyzing the force on UAV during landing, a parachute landing model of UAV was established and emulationally analyzed. It is shown that the landing track was obtained and thus this landing system was satisfied.

关 键 词：无人机 伞降回收 风场 

分 类 号：TP301.6[自动化与计算机技术—计算机系统结构]