发明名称 Smart electric taxi path control
摘要 An aircraft taxi control system may include a motor connected to drive a landing gear wheel of the aircraft. A motor controller may be connected to control speed of the motor. The system may also include an aircraft taxi route database, an aircraft position determination unit; an aircraft performance database and a processor configured to a) integrate signals from the aircraft taxi route database, the aircraft position determination unit and aircraft performance database, and b) produce a motor deceleration signal to the motor controller when the aircraft arrives at a predetermined distance from a predetermined location so that the aircraft arrives at the location traveling at a desired speed.
申请公布号 US9293055(B2) 申请公布日期 2016.03.22
申请号 US201414325565 申请日期 2014.07.08
申请人 HONEYWELL INTERNATIONAL INC. 发明人 Nutaro Joseph;Jackson Patrick;Sims Jay
分类号 G01C23/00;G08G5/06;B64C25/34;B64C25/40;B64C25/42;G05D1/00;G05D13/62 主分类号 G01C23/00
代理机构 Shimokaji IP 代理人 Shimokaji IP
主权项 1. An aircraft taxi control system comprising: at least one motor connected to drive at least one landing gear wheel of the aircraft; a motor controller connected to control speed of the at least one motor; an aircraft taxi route database; an aircraft position determination unit; an aircraft performance database; a processor configured to, a) integrate signals from the aircraft taxi route database, the aircraft position determination unit and aircraft performance database, andb) produce a motor deceleration signal, based on the signals integrated in step (a), to the motor controller when the aircraft arrives at a predetermined distance from a predetermined location so that the aircraft arrives at the predetermined location traveling at a desired speed without a need for manual speed adjustment by a pilot of the aircraft.
地址 Morris Plains NJ US