Abrégé

The invention relates to a flight state system (20) for ascertaining a flight state of a paraglider (50, 50′) which comprises a canopy (51) with two canopy ends (52) and which carries a load (53) during intended use. Thereby, the flight state system comprises a sensor arrangement (S1, S2, S3) for ascertaining a first distance (d1) between the canopy ends (52) and/or at least a second distance (d2, d3) between a canopy end (52) and the load (53). Furthermore, the flight state system comprises an evaluation unit (37) which ascertains the flight state using the first distance (d1) and/or the second distances (d2, d3). The invention further relates to an evaluation system and/or control system (40), a paraglider (50, 50′) and a method for ascertaining a flight state of a paraglider (50, 50′).

Classes IPC  ?

• B64D 17/62 - Déploiement des parachutes
• B64C 31/02 - Planeurs, p. ex. planeurs de vol à voile

Abrégé

A paraglider controller for controlling a paraglider drive, in particular an electric ascent aid, for a paraglider. The paraglider controller comprises a UI connection interface for sending and/or receiving user commands comprising a voice signal. Optionally, the ascent aid control further comprises a flight data interface for receiving flight data. Furthermore, the ascent aid control comprises an evaluation unit for evaluating received user commands and optionally flight data, wherein a user signal is output via the UI connection interface and/or a control signal is output via a control interface. An input and/or an output of user commands is thereby carried out using the UI connection interface by means of the speech signal.

Classes IPC  ?

• B64C 31/036 - Aéronefs du type pendulaireAéronefs du type ultra-léger avec des ailes du type parachute
• G05D 1/2285 - Dispositions d’entrée de commande situées à bord de véhicules sans pilote utilisant des commandes vocales ou gestuelles
• G05D 109/20 - Aéronefs, p. ex. drones