The invention relates to the field of unmanned aerial vehicles, in particular to a coaxial unmanned aerial vehicle control method. A navigation flight control computer A and a navigation flight control computer B are arranged; the ground station can be in communication connection with a ground remote control and telemetering transceiver, and is respectively in communication connection with the navigation flight control computer A and the navigation flight control computer B through a main remote control telemetering channel and a backup remote control telemetering channel; the ground remote control and a telemetering transceiver is in communication connection with a remote controller II, and the remote controller II can control an engine, a longitudinal dual-redundancy electric steering engine, a transverse dual-redundancy electric steering engine, a course dual-redundancy electric steering engine, a total distance dual-redundancy electric steering engine and an accelerator dual-redundancy electric steering engine of the unmanned aerial vehicle so as to control the form of the unmanned aerial vehicle; an air pressure sensor can provide atmosphere information for the navigation flight control computer A and the navigation flight control computer B through the atmosphere data computer.
本发明涉及无人机领域,尤其涉及一种共轴无人机控制方法。导航飞控计算机A和导航飞控计算机B,地面站能够和地面遥控、遥测收发射机通信连接,通过主遥控遥测通道和备份遥控遥测通道分别通信连接着导航飞控计算机A和导航飞控计算机B;地面遥控、遥测收发射机通信连接着遥控二,遥控二能够控制无人机的发动机、纵向双余度电动舵机、横向双余度电动舵机、航向双余度电动舵机、总距双余度电动舵机、油门双余度电动舵机进行控制进而操纵飞机形态;空气压力传感器通过大气数据计算机能够给导航飞控计算机A和导航飞控计算机B提供大气信息。
Coaxial unmanned aerial vehicle control method
一种共轴无人机控制方法
2021-11-12
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / F41H Panzerung , ARMOUR |