文献类型：专利

英文题名：Control system of four-rotary wing aircraft, has controller which is respectively connected with flying posture detector and four-rotary wing aircraft motor and which is connected to one end of wireless communication device

作者：HU K;LI Y;FU Z

机构：[1]UNIV EAST CHINA SCI & TECHNOLOGY

申请号：CN106919179-A

申请日：2017-04-28

公开日：2017-07-04

语种：英文

收录：DERWENT

摘要：NOVELTY - The control system has a wireless communication device (3) whose one end is communicated with an upper computer (5) through a universal serial bus (USB) communication serial port (4). Other end of the wireless communication device is connected to a controller (1). The controller is respectively connected with a flying posture detector (2) and four-rotary wing aircraft motor (6). USE - Control system of four-rotary wing aircraft. ADVANTAGE - The control system which has stable and fast operation of the four-rotary wing aircraft, which performs remote monitoring and which improves the anti-interference ability with technical support is achieved by the improved control system. DETAILED DESCRIPTION - An INDEPENDENT CLAIM is included for a control method for a four-rotary wing aircraft. DESCRIPTION OF DRAWING(S) - The drawing shows a block diagram of the control system of the four-rotary wing aircraft. (Drawing includes non-English language text) Controller (1) Flying posture detector (2) Wireless communication device (3) USB communication serial port (4) Upper computer (5) Four-rotary wing aircraft motor (6)