Fast attitude error correction

An aerial vehicle platform includes an aerial vehicle, a gimbal coupled to the aerial vehicle, and a camera mounted to the gimbal. An attitude sensing system includes an inertial measurement unit to sense attitude and an attitude adjustment module to generate an attitude adjustment for adjusting the...

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Bibliographic Details
Main Authors Bruneau, Garance, Gohl, Pascal, Murguet, Axel, Gubler, Thomas
Format Patent
LanguageEnglish
Published 23.07.2019
Subjects
ACCESSORIES THEREFOR
AEROPLANES
AIRCRAFT
APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USINGWAVES OTHER THAN OPTICAL WAVES
APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FORPROJECTING OR VIEWING THEM
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
CINEMATOGRAPHY
COSMONAUTICS
ELECTRIC COMMUNICATION TECHNIQUE
ELECTRICITY
ELECTROGRAPHY
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
GYROSCOPIC INSTRUMENTS
HELICOPTERS
HOLOGRAPHY
MEASURING
MEASURING DISTANCES, LEVELS OR BEARINGS
NAVIGATION
PARACHUTES
PERFORMING OPERATIONS
PHOTOGRAMMETRY OR VIDEOGRAMMETRY
PHOTOGRAPHY
PHYSICS
PICTORIAL COMMUNICATION, e.g. TELEVISION
SURVEYING
TESTING
TRANSPORTING
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Summary:An aerial vehicle platform includes an aerial vehicle, a gimbal coupled to the aerial vehicle, and a camera mounted to the gimbal. An attitude sensing system includes an inertial measurement unit to sense attitude and an attitude adjustment module to generate an attitude adjustment for adjusting the sensed attitude to compensate for drift error.
Bibliography:Application Number: US201715788769