公开(公告)号：US20160117935A1

公开(公告)日：2016-04-28

申请号：US14502957

申请日：2014-09-30

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Subash Samuthirapandian ,  Markus A. Johnson

IPC: G08G5/04 ,  G08G5/06 ,  B64C25/34 ,  B64C25/40

CPC classification number: G08G5/04 ,  B64C25/34 ,  B64C25/405 ,  B64D45/00 ,  G08G5/0008 ,  G08G5/0021 ,  G08G5/0078 ,  G08G5/0091 ,  G08G5/045 ,  G08G5/065 ,  Y02T50/823

Abstract: An electric taxi motive control system of a first aircraft comprises a first aircraft position determining system configured to generate a first aircraft position signal, a first aircraft receiver, configured to receive transmissions of a second aircraft position signal, a first aircraft pilot interface configured to accept an input indicative of a first aircraft desired speed, and a first aircraft electronic controller configured to; determine a aircraft separation distance indicative of the distance between the first aircraft and the second aircraft, compare the aircraft separation distance with a safe distance value; and generate a modified first aircraft commanded speed signal when the aircraft separation distance is less than the safe distance value.

Abstract translation: 第一飞行器的电动出租车动力控制系统包括被配置为产生第一飞行器位置信号的第一飞行器位置确定系统，被配置为接收第二飞行器位置信号的传输的第一飞行器接收器，被配置为接受的第一飞行器接口 指示第一飞行器期望速度的输入;以及第一飞行器电子控制器，其被配置为： 确定指示第一飞机和第二飞机之间的距离的飞机间隔距离，将飞机间隔距离与安全距离值进行比较; 并且当飞行器分离距离小于安全距离值时，生成修改的第一飞机命令速度信号。

公开(公告)号：US09640082B2

公开(公告)日：2017-05-02

申请号：US14502957

申请日：2014-09-30

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Subash Samuthirapandian ,  Markus A. Johnson

IPC: G08G5/04 ,  B64C25/40 ,  G08G5/06 ,  B64C25/34 ,  B64D45/00

CPC classification number: G08G5/04 ,  B64C25/34 ,  B64C25/405 ,  B64D45/00 ,  G08G5/0008 ,  G08G5/0021 ,  G08G5/0078 ,  G08G5/0091 ,  G08G5/045 ,  G08G5/065 ,  Y02T50/823

Abstract: An electric taxi motive control system of a first aircraft comprises a first aircraft position determining system configured to generate a first aircraft position signal, a first aircraft receiver, configured to receive transmissions of a second aircraft position signal, a first aircraft pilot interface configured to accept an input indicative of a first aircraft desired speed, and a first aircraft electronic controller configured to; determine a aircraft separation distance indicative of the distance between the first aircraft and the second aircraft, compare the aircraft separation distance with a safe distance value; and generate a modified first aircraft commanded speed signal when the aircraft separation distance is less than the safe distance value.