AUTOMATIC PILOTING DEVICES HELICOPTERS

Brand Owner Address Description
STABLELIGHT THALES AVS FRANCE SAS 75-77 AVENUE MARCEL DASSAULT MERIGNAC 33700 France Automatic piloting devices for helicopters and airplanes; Navigation, guidance and stability devices for helicopters and airplanes; Electronically controlled devices for aerodynamic flight control in airplanes; Automatic flight control devices for piloting helicopters and airplanes; Automatic electric flight control and command systems comprised of software and hardware for flight control for helicopters and airplanes; automatic fibre-optic flight control and command systems comprised of software and hardware for flight control for helicopters and airplanes; On-board instruments providing information to the pilot on in-flight situation awareness of the helicopter; Helicopter and aircraft flight parameter control equipment namely, digital transmitters; Helicopter and aircraft navigation apparatus and instruments; Avionics instruments, related equipment and related systems, namely, digital transmitters; Telecommunication equipment, namely, fiber-optic transceivers, fiber optic repeaters, converters and optimizers, wave division multiplexers, free-space optics transmission systems, switches including Ethernet switches and routers; Data processing equipment; computers; computer hardware, and peripherals adapted for use with computers; Downloadable or recorded software for flight control for helicopters and airplanes; Flight simulators; Sensors namely, electronic sensors for helicopters and airplanes; Detectors namely, electronic detectors for helicopters and airplanes; Receivers namely, electronic receivers for helicopters and airplanes;Adaptation and conversion of hardware for machines and flight equipment; Adaptation, conversion, replacement and installation of autopilot hardware devices for helicopters and airplanes; Installation, maintenance and updating of all parts and components of autopilot hardware devices for helicopters and aircraft;STABLE LIGHT;Scientific and technological services namely, research and design in the field of helicopter and aircraft autopilot devices and aircraft aerodynamic flight control devices; Industrial analysis and research services in the field of helicopter and aircraft autopilot devices and aircraft aerodynamic flight control devices; Technical consulting in relation to computer technology consultancy in the fields of helicopter and aircraft autopilot devices and aircraft aerodynamic flight control devices; Consulting, research, design, expertise consulting and testing services in relation to computer technology consultancy all in the field of helicopter and aircraft autopilot devices and aircraft aerodynamic flight control devices; Quality control services for others; Engineering consulting services; Software design and development; Quality control to determine conformity with certification standards; Product quality testing to determine conformity with certification standards; Analysis and evaluation of products to determine conformity with certification standards; all of the above services being performed in the context of the supply of helicopter and aircraft autopilot devices and aircraft aerodynamic flight control devices; Testing, analysis and evaluation of replacement services for helicopter and aircraft autopilot devices and for aircraft aerodynamic flight control devices to determine conformity with certification standards;
 

Where the owner name is not linked, that owner no longer owns the brand

    
Technical Examples
  1. Methods, systems, and computer program products are provided for navigating a UAV that include piloting the UAV, under control of a navigation computer, in accordance with a navigation algorithm. While piloting the UAV, embodiments include reading from the GPS receiver a sequence of GPS data, anticipating a future position of the UAV, identifying an obstacle in dependence upon the future position, selecting an obstacle avoidance algorithm, and piloting the UAV in accordance with an obstacle avoidance algorithm. Identifying an obstacle in dependence upon the future position may include comprises retrieving obstacle data from a database in dependence the future position. Identifying an obstacle in dependence upon the future position may also include depicting an anticipated flight of the UAV with 3D computer graphics in dependence upon the future position and identifying an obstacle in dependence upon the depiction of the anticipated flight.