Active side lever device and aircraft control system

The embodiment of the invention discloses an active side rod device and an aircraft control system, and the active side rod device comprises a mounting frame, a first rotating part, a second rotating part, a connector assembly, a control rod, a first force feedback assembly, a second force feedback...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	HUANG XU, GUO HAIXIN, YOU SIQI, GUAN CHEN, LI JIAN, JU HAOCHEN
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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