DEFAULT IN-DETENT VERTICAL SPEED/ALTITUDE HOLD

A rotorcraft (101, Figure 1) including a flight control computer (FCC) (205) providing a vertical speed hold for the rotorcraft (101), a collective control (233), and a collective trim motor (213) connected to the collective control (233). The collective trim motor (213) moves the collective control...

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Bibliographische Detailangaben

Hauptverfasser:	WORSHAM, Robert Earl, KLEIN, Morganne Cody, BOTHWELL, Christopher Mike, ALFRED, Jillian Samantha, GILLETT, Luke Dafydd, KIM, Sung Kyun
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CONTROLLING COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING
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