首页> 外国专利> Unmanned aerial vehicle and method for safely landing an unmanned aerial vehicle

Unmanned aerial vehicle and method for safely landing an unmanned aerial vehicle

机译：无人机和用于安全降落无人机的方法

页面导航

摘要
著录项
相似文献

摘要

An unmanned aerial vehicle with lift and propulsion system and a flight control system and method. The flight control system has a flight control unit, a navigation system, a communication system and an actuator system. The flight control unit can calculate, based on data from the navigation system and/or data of a ground control station, control commands which can be fed to the actuator system for actuating the lift and propulsion system. The ground control station is configured to control and/or monitor the aerial vehicle. The aerial vehicle has a monitoring unit to monitor the communication system to determine whether all the communication links are interrupted. The monitoring unit can cause the flight control unit to land the aerial vehicle safely at a suitable landing site based on stored data relating to current flight conditions and nearby landing sites.

机译：一种具有升力和推进系统的无人飞行器以及飞行控制系统和方法。该飞行控制系统具有飞行控制单元，导航系统，通信系统和致动器系统。飞行控制单元可以基于来自导航系统的数据和/或地面控制站的数据来计算控制命令，该控制命令可以被馈送到致动器系统以致动升力和推进系统。地面控制站被配置为控制和/或监视飞行器。该飞行器具有监视单元，以监视通信系统以确定是否所有通信链路都被中断。监视单元可以基于与当前飞行状况和附近的着陆点有关的存储数据，使飞行控制单元将飞行器安全地着陆在合适的着陆点。

著录项

公开/公告号US10319246B2

专利类型
公开/公告日2019-06-11

原文格式PDF
申请/专利权人 AIRBUS DEFENCE AND SPACE GMBH;
展开▼

申请/专利号US201615280436
发明设计人 MANFRED HIEBL;
展开▼

申请日2016-09-29
分类号G05D1;G05D1/02;G05D1/10;G08G5;B64C39/02;G01C21;G08G5/06;G05D1/06;H04B7/155;H04L29/08;
国家 US
入库时间 2022-08-21 12:16:47

相似文献

专利
外文文献
中文文献