Inventor · Fauconnières, FR

Jacques Coatantiec

16Patents
5h-index
15Co-inventors
59Inventor score

Filing activity: Sep 24, 2002 → Apr 3, 2020

Most-cited inventions

PatentTitleAreaCited byStatus
US6982669B2 Hybrid inertial navigation system with improved integrity Physics 46 Expired
US7409289B2 Device for monitoring the integrity of information delivered by a hybrid INS/GNSS system Physics 40 Expired
US7711482B2 Hybrid INS/GNSS system with integrity monitoring and method for integrity monitoring Physics 16 Active
US8566033B2 Method for determining the position of a mobile body at a given instant and for monitoring the integrity of the position of said mobile body Physics 5 Active
US9146322B2 Hybrid system and device for calculating a position and for monitoring its integrity Physics 5 Active
US8878722B2 Method and system for determining navigation parameters of an aircraft Physics 4 Active
US8311728B2 Navigation system using hybridization by phase measurements Physics 4 Active
US7689357B2 Closed loop hybridising device with monitoring of the measurement integrity Physics 2 Active
US9726499B2 Method of determining a radius of protection associated with a navigation parameter of a hybrid inertial navigation system, and associated system Physics 2 Active
US10908296B2 Method for calculating a speed of an aircraft, method for calculating a protection radius, positioning system and associated aircraft Physics 1 Active
US8655511B2 Method and system for determining the attitude of an aircraft by multi-axis accelerometric measurements Physics 1 Active
US12098922B2 Inertial reference unit and system with enhanced integrity and associated integrity-checking methods Physics 0 Active
US10094932B2 Method and integrity verification device location information obtained by at least two satellite geolocation devices Physics 0 Active
US9550579B2 Method of estimation of the speed of an aircraft relative to the surrounding air, and associated system Physics 0 Active
US11788842B2 Hybrid AHRS system comprising a device for measuring the integrity of the calculated attitude Physics 0 Active
US9828111B2 Method of estimation of the speed of an aircraft relative to the surrounding air, and associated system Physics 0 Active

Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.