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 |