ASSISTED TAKE-OFF METHOD FOR AIRCRAFT

A reference value is arbitrarily selected from a range of possible aircraft rotation speeds. A position of a trimmable horizontal stabilizer is angled in accordance with a centering of the reference value. A deviation between the reference value and an accelerating speed value of the aircraft is det...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	MATHIEU, GERARD, DELAPLACE, FRANCK, LE TRON, XAVIER
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	CONTROLLING PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
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