ASCERTAINING A FLIGHT STATE, AND CONTROLLING A PARAGLIDER

ASCERTAINING A FLIGHT STATE, AND CONTROLLING A PARAGLIDER

The invention relates to a flight state system (20) for ascertaining the flight state of a paraglider (50, 50') which comprises a canopy (51) with two canopy ends (52) and which carries a load (53) when operated as intended. The flight state system comprises a sensor assembly (S1, S2, S3) for a...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: MEIßNER, Marius, STÄDTLER, Jürgen
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
HELICOPTERS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:The invention relates to a flight state system (20) for ascertaining the flight state of a paraglider (50, 50') which comprises a canopy (51) with two canopy ends (52) and which carries a load (53) when operated as intended. The flight state system comprises a sensor assembly (S1, S2, S3) for ascertaining a first distance (d1) between the canopy ends (52) and/or at least one second distance (d2, d3) between one canopy end (52) and the load (53). Additionally, the flight state system comprises an analysis unit (37) which ascertains the flight state using the first distance (d1) and/or the second distance (d2, d3). The invention additionally relates to an analysis system and/or a control system (40), to a paraglider (50, 50'), and to a method for ascertaining the flight state of a paraglider (50, 50').