Invention Application
US20050021193A1 Fly-by-wire control system for an aircraft comprising detection of pilot induced oscillations and a control for such a system 审中-公开
一种用于飞行器的线控控制系统,包括检测导频感应振荡和这种系统的控制

Fly-by-wire control system for an aircraft comprising detection of pilot induced oscillations and a control for such a system
Abstract:
Fly-by-wire control system for an aircraft comprising detection of pilot induced oscillations and a control for such a system. According to the invention, provision is made for the pivotings of said control (2) to be damped by controllable damping means (15, 16) controlled by means (7) detecting oscillations corresponding to pilot induced oscillations.
Information query
Patent Agency Ranking
0/0