Airplane active side lever system

Abstract

The present invention discloses an airplane active side lever system. The airplane active side lever system comprises a monitoring module and a side level module. The monitoring module communicates the side level module through a serial port communication mode, and the format and the length of a communication data packet are constant. The monitoring module is able to obtain the real-time state of data of a control stick and set the work modes of the side level module, wherein the work modes include a follow-up mode, a balancing mode, an active mode and a passive mode. The balancing mode, the active mode and the passive mode can be switched by inputting instructions through the monitoring module or be switched by buttons on a side lever handle, the balancing mode and the active mode are switched by a balancing switch at the top of the side level handle, and the passive mode and the active mode are switched by a switching switch at the side surface of the side lever handle; and the monitoring module sends instructions to the follow-up mode which is switched in the active mode and the balancing mode.

Description

technical field [0001] The invention relates to an aircraft control system, in particular to an aircraft active side stick system. Background technique [0002] The human-sensing system of the aircraft can make the pilot have a sense of control when manipulating the aircraft, and can affect the handling performance of the aircraft. It is a very important part of the aircraft control system. Fly-by-wire fly-by-wire control systems are used in most aircraft today, where a spring-loaded passive control stick system forms the human-sensing system for these aircraft. This type of control stick has a very simple structure, is very convenient to install, and is also very stable to operate, but the biggest disadvantage is that the force of the control stick and the displacement of the stick is a fixed proportional relationship, which cannot reflect the flight state of the aircraft; The pilot cannot feel the flight state of the aircraft, and the flight quality and handling quality o...

AI Technical Summary

Problems solved by technology

[0003] The existing active side stick system, on the same aircraft model, cannot customize the stick force-displacement curve according to different flight tasks, resulting in the active side stick not being able to exert greater advantages; the existing active side stick generally removes the passive mode, or adopts step Incoming motor switching mode

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