发明名称 CONTROL DEVICE FOR UNMANNED HELICOPTER
摘要 PROBLEM TO BE SOLVED: To provide a control device for an unmanned helicopter capable of performing the stable turning flight even when the helicopter is under strong wind or the weight of a helicopter body 3 is large while employing the configuration to facilitate the steering operation. SOLUTION: A maximum turn bank angle setting means 23 is provided, which obtains the maximum turning bank angle allowing the stable flight in the present flight condition of the helicopter body 3. A turn yaw rate correction means 24 is provided, which set the turn yaw rate of the helicopter body 3 so that the actual turn bank angle is not larger than the maximum bank angle when the actual bank angle of the helicopter body 3 is larger than the maximum turn bank angle. COPYRIGHT: (C)2005,JPO&NCIPI
申请公布号 JP2005247009(A) 申请公布日期 2005.09.15
申请号 JP20040056499 申请日期 2004.03.01
申请人 YAMAHA MOTOR CO LTD 发明人 NAKAMURA KATSU
分类号 B64C13/20;B64C27/04;B64C39/02;G05D1/10;(IPC1-7):B64C13/20 主分类号 B64C13/20
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