| 发明名称 |
METHOD OF MANAGING A STEERING COMMAND FOR A STEERABLE PORTION OF AIRCRAFT LANDING GEAR |
| 摘要 |
The invention relates to a method of managing a steering command for a steerable portion 3 of nose landing gear 2 of an aircraft 1, the method implementing servo-control to servo-control a steering actuator 6 to an angle position setpoint θset for the steerable portion 3, the servo-control including calculating an error ε by subtracting a reference angle θest from the angle position setpoint θset. According to the invention, the reference angle θest is an angle determined by calculation as a function of a longitudinal speed Vlong and a yaw rate τ of the aircraft 1. |
| 申请公布号 |
US2014156113(A1) |
申请公布日期 |
2014.06.05 |
| 申请号 |
US201313779397 |
申请日期 |
2013.02.27 |
| 申请人 |
MESSIER-BUGATTI-DOWTY |
发明人 |
BENMOUSSA Michael;POIRET David;FRAVAL Jerome |
| 分类号 |
B64C19/00 |
主分类号 |
B64C19/00 |
| 代理机构 |
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代理人 |
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| 主权项 |
1. A method of managing a steering command for a steerable portion (3) of nose landing gear (2) of an aircraft (1), the method implementing servo-control to servo-control a steering actuator (6) to an angle position setpoint (θset) for the steerable portion (3), the servo-control including calculating an error (ε) by subtracting a reference angle (θest) from the angle position setpoint (θset), the method being characterized in that the reference angle (θest) is an angle determined by calculation as a function of a longitudinal speed (Vlong) and a yaw rate (τ) of the aircraft (1).
|
| 地址 |
Velizy-Villacoublay FR |
