An onboard system for controlling flight of an unmanned aerial vehicle. The system comprises: a flight management system configured for controlling flight of the unmanned aerial vehicle; a mission control module configured to send commands to the flight management system for guiding the unmanned aerial vehicle to perform a mission; a safety module configured to communicate commands to the flight management system for guiding the unmanned aerial vehicle to fly in a safe mode; a communication control component which is switchable between a mission state in which the flight management system receives commands from the mission control module and a safety state in which the flight management system receives commands from the safety module; and a monitor module configured to determine whether a trigger condition warranting a change in mode is present or not and to cause the communication control component to switch from the mission state to the safety state when the trigger condition is present.
Unmanned Aerial Vehicle Flight Control System
2017-09-21
Patent
Electronic Resource
English
IPC: | G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge / 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 |
European Patent Office | 2022
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