公开(公告)号：US11169543B2

公开(公告)日：2021-11-09

申请号：US16435239

申请日：2019-06-07

Applicant: THALES

Inventor： Romain Lamour ,  Frédéric Berger ,  François Colonna ,  Marianne Cazes

IPC: G05D1/10 ,  B64C13/18

Abstract: A conversion device for converting a guidance setpoint signal from an aircraft guidance system for at least one control axis, for example, into a control signal for an avionics system such as an aircraft stabilization system. The device may include comprising an acquisition module designed to acquire the guidance setpoint signal. The device may further include a generation module designed to generate the control signal from the acquired guidance setpoint signal. The control signal may include at least two command pulses. The generation module may be designed to calculate the duration between two consecutive command pulses depending on a corresponding value of the acquired guidance setpoint signal.