An aeroplane attitude indicator device includes a mobile rod which includes a first end connected by a link to a support fastened to the aeroplane and a second end to which is connected a moving body, at least one actuator for controlling the motions of the rod, and a system for piloting the at least one actuator as a function of information originating from an attitude detection system of the aeroplane, so as to orient the rod in a vertical direction. The assembly of rod and moving body correspond to a pendulum-like artifact. Also described is an aeroplane cockpit equipped with an attitude indicator device.
Aircraft attitude indicator device
2017-05-09
Patent
Electronic Resource
English
INTUITIVE DISPLAY OF ANGLE OF ATTACK GUIDANCE ON AIRCRAFT ATTITUDE INDICATOR
European Patent Office | 2018
|INTUITIVE DISPLAY OF ANGLE OF ATTACK GUIDANCE ON AIRCRAFT ATTITUDE INDICATOR
European Patent Office | 2018
|'Light Bar' Attitude Indicator
NTIS | 1981
|ATTITUDE CHANGING DEVICE, UNMANNED AIRCRAFT, AND ATTITUDE CHANGING METHOD
European Patent Office | 2021
|