| 直升机加载抑制多余力控制研究 |
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| 引用本文： | 王新民,刘卫国.直升机加载抑制多余力控制研究[J].机床与液压,2005(7):142-143,86. |
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| 作者姓名： | 王新民 刘卫国 |
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| 作者单位： | 西北工业大学自动化学院,西安,710072 |
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| 摘 要： | 针对直升机旋翼加载多余力问题，对耦合模型进行了分析，基于结构不变性原理，讨论了解耦通道的设计，给出了不同的结构和参数配置情况及其多余力消除效果，其结论用于实际系统调试参考。
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| 关 键 词： | 直升机旋翼加载 多余力 结构不变性原理 |
| 文章编号： | 1001-3881(2005)7-142-2 |
Research on Eliminating Extra Torque in Loading System of Helicopter Rotor |
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| WANG Xin-min,LIU Wei-guo.Research on Eliminating Extra Torque in Loading System of Helicopter Rotor[J].Machine Tool & Hydraulics,2005(7):142-143,86. |
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| Authors: | WANG Xin-min LIU Wei-guo |
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| Abstract: | The couple model was described in order to eliminate the extra torque in loading system of helicopter rotor.A feedforward compensation was discussed,different structure parameters and effects as the feedforward to eliminate extraneous force were investigated and compared,the conclusion is useful for loading system experiment. |
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| Keywords: | Helicopter rotor loading Extra torque Structure-invariable theory |
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