发明名称 |
Gyroscope for remote-controlled helicopters |
摘要 |
A gyroscope suitable for a remote-controlled helicopter is provided that can improve the control characteristics to a disturbance factor such as wind as well as the response characteristics under yaw-axis control in a correct pitch operation. The angular velocity detection signal from the yaw-axis angular velocity sensor 10 is added to the yaw-axis control signal and the angular velocity reference value from the controlling gear. The PID controller 2 receives the resultant addition signal. The control signal from the PID controller 2 is added to the correct pitch control signal and the yaw-axis control signal sent via the correct pitch to yaw-axis control mixing unit 3. The actuator 6 receives the resultant addition signal and controls the yaw-axis driving unit 7. The yaw-axis angular velocity detection sensor 10 detects the angular velocity around the yaw-axis of the airframe 9.
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申请公布号 |
US6227482(B1) |
申请公布日期 |
2001.05.08 |
申请号 |
US19990264675 |
申请日期 |
1999.03.09 |
申请人 |
FUTABA DENSHI KOGYO KABUSHIKI KAISHA |
发明人 |
YAMAMOTO MICHIO |
分类号 |
A63H27/133;A63H30/00;A63H30/04;B64C39/02;G01C19/02;G01C19/56;G01P13/02;G05D1/08;(IPC1-7):B64C13/16;B64C27/57 |
主分类号 |
A63H27/133 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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