公开(公告)号：US20190324455A1

公开(公告)日：2019-10-24

申请号：US13869413

申请日：2013-04-24

Applicant: Thales

Inventor： Rodolphe DEVAUREIX ,  Arnaud BONNAFOUX ,  Jerome BIRRE

IPC: G05D1/00 ,  G05D1/02 ,  B64D45/00 ,  G06F17/11 ,  G06F9/54 ,  G06F9/30 ,  G06F16/9035

Abstract: An automatic piloting system intended for an aircraft comprising an aircraft signals acquisition module, a module for interfacing with the crew, and a module for processing the output signals, comprises: a generic software kernel for automatic piloting aboard the aircraft, comprising several parametrizable elementary cells, a parametrization tool for the generic software kernel, able to transform an operational need of the automatic piloting system, expressed by means of a configuration file in accordance with a predetermined configuration domain DC, into a database of binary parameters DB able to parametrize the generic software kernel; each cell being parametrized by the database DB, and means for loading and storage aboard the aircraft of the database DB.

公开(公告)号：US20130345907A1

公开(公告)日：2013-12-26

申请号：US13917487

申请日：2013-06-13

Applicant: THALES

Inventor： Yannick MERET ,  Arnaud BONNAFOUX ,  Christophe SIMON

IPC: B64C13/16

CPC classification number: B64C13/16 ,  B64C13/18 ,  B64C13/30 ,  G05D1/0808

Abstract: A method for automatic yaw axis control in aircraft with mechanical controls, said aircraft including a yaw actuator to control orientation of a yaw control surface and deliver a measured value of the torque on the control surface, a yaw trim actuator driving movement of a yaw trim control surface limiting the force applied by the yaw actuator to orient the yaw control surface, and sensors supplying an estimate of a lateral yaw force, includes calculating a setpoint value for the position of the yaw control surface determined by the estimated lateral force, an estimated torque of the yaw actuator determined by the measured value of the torque of the yaw actuator and a measured position of the yaw control surface, the estimated torque calculated having a lower oscillation dynamic range than the measured torque, and a trim command for activating/deactivating the yaw trim actuator determined by the estimated torque.

Abstract translation: 一种用于具有机械控制的飞行器中的自动偏航轴控制的方法，所述飞行器包括偏航致动器，以控制偏航控制表面的方位并将扭矩的测量值传递到控制表面上;偏航调整致动器驱动偏航装饰 控制表面限制由偏航致动器施加的力以定向偏航控制表面，以及提供横向偏转力的估计的传感器包括计算由所估计的横向力确定的偏航控制表面的位置的设定值，估计 由偏航致动器的扭矩的测量值和偏航控制表面的测量位置确定的偏航致动器的扭矩，计算出的具有比测量的扭矩更低的振动动态范围的估计转矩以及用于激活/停用的修剪命令 由所估计的扭矩确定的偏航修正致动器。