METHOD OF CONTROLLING A BUOYANCY SYSTEM FOR AN AIRCRAFT, AND A CONTROL SYSTEM IMPLEMENTING SAID METHOD

METHOD OF CONTROLLING A BUOYANCY SYSTEM FOR AN AIRCRAFT, AND A CONTROL SYSTEM IMPLEMENTING SAID METHOD

The present invention relates to a method of controlling a buoyancy system for an aircraft, wherein the buoyancy system including automatic trigger means and the method consists in: a) determining the roll angle and the pitching angle of the aircraft; b) verifying whether − R<

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Bibliographische Detailangaben
1. Verfasser: FILIAS FRANCOIS-XAVIER
Format: Patent
Sprache:eng
Schlagworte:
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES IN GENERAL
VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISEPROVIDED FOR
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Beschreibung
Zusammenfassung:The present invention relates to a method of controlling a buoyancy system for an aircraft, wherein the buoyancy system including automatic trigger means and the method consists in: a) determining the roll angle and the pitching angle of the aircraft; b) verifying whether − R<