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REMOTE FLIGHT CONTROL SYSTEM FOR PILOTLESS HELICOPTER

机译:无人直升机遥控飞行控制系统

摘要

PURPOSE: To prevent a remote flight control system of a pilotless helicopter having a function of increasing the stability of the angular speed in one, two or three axial directions or a function of holding the attitude from the automatic vibtation and resonance phenomenon of the helicopter body on the ground which may be generated in the taking-off and landing. ;CONSTITUTION: A mixing amplifier 4 of flight controller provided with a taking- off and landing detecting means 9 for detecting whether a helicopter is taking- off or landing changes over the level of a signal Se' mixed with a maneuvering signal Sb to zero or small one when the output Sd of the taking-off and landing detecting means 9 is under the landing condition. On the other hand, a plurality of signal processing sections differing in the signal processing properties may be provided to selectively change over these outputs for mixing according to the Sd. A mechanical switch or pressure sensor turned on/off by its own weight is provided on a skid of the hericopter for example to constitute the taking-off and landing detecting means 9.;COPYRIGHT: (C)1996,JPO
机译:目的:为了防止无人驾驶直升机的远程飞行控制系统具有增加在一个,两个或三个轴向上角速度的稳定性的功能,或者具有保持姿态免受直升机机体的自动振动和共振现象的作用的功能在起飞和降落时可能会产生的地面上。 ;组成:飞行控制器的混合放大器4,具有起飞和降落检测装置9,用于检测直升机的起飞或降落是否在与操纵信号Sb混合的信号Se'的电平上变为零或起飞和着陆检测装置9的输出Sd处于着陆状态时,小。另一方面,可以提供信号处理特性不同的多个信号处理部,以根据Sd选择性地切换这些输出以进行混合。在直升机的滑橇上设置有通过自重打开/关闭的机械开关或压力传感器,例如,它构成了起飞和降落检测装置9;版权所有:(C)1996,JPO

著录项

  • 公开/公告号JPH0848297A

    专利类型

  • 公开/公告日1996-02-20

    原文格式PDF

  • 申请/专利权人 JAPAN AVIATION ELECTRON IND LTD;

    申请/专利号JP19940184692

  • 发明设计人 YOKOTA KOICHI;

    申请日1994-08-05

  • 分类号B64C13/20;A63H27/133;A63H30/00;G05D1/00;G05D1/08;

  • 国家 JP

  • 入库时间 2022-08-22 03:57:31

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