High altitude parachute navigation flight computer

G - Physics – 01 – C

Patent

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Details

G01C 23/00 (2006.01)

Patent

CA 2556009

A navigational computer design (10) for high altitude and other similar navigational needs includes a processor (52), which receives as input signals from navigational and navigational related sensors such as a GPS (60), compass (59), inertial measurement unit (56) and sensors. Processor utilizes the navigational information to provide a display (110) to the user indicating present navigational positional information as well as providing a flight path (310) to follow to the target. The navigational computer (10) includes a device that enables it to operate in a peer-to-peer network with other similar navigational computers such that during use, users may track one another. Once on the ground, the navigational computer (10) may be used to continue navigation.

La présente invention concerne un modèle d'ordinateur de navigation (10) répondant aux besoins de la navigation à haute altitude ou analogue. Il comporte un processeur qui reçoit ses signaux d'entrée de capteurs de navigation et de capteurs se rapportant à la navigation tels qu'un GPS (60), un compas (59), une centrale inertielle (56) et des capteurs. Les informations de navigation permettent au processeur de fournir à l'utilisateur une image (110) donnant une estime sur carte et lui proposant un tracé de route à suivre (310) pour arriver au but. Cet ordinateur de navigation (10) comporte un dispositif qui lui permet de fonctionner dans un réseau d'homologue à homologue avec d'autres ordinateurs de navigation semblable, de façon que, pendant l'utilisation, les utilisateurs puissent se pister mutuellement. Revenu au sol, l'ordinateur de navigation (10) pour servir pour continuer la navigation.

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