| 基于DMC-PID复合控制的无人直升机飞控系统设计 |
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| 引用本文： | 单俊杰,段镖,赖水清.基于DMC-PID复合控制的无人直升机飞控系统设计[J].直升机技术,2011(4):30-34. |
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| 作者姓名： | 单俊杰 段镖 赖水清 |
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| 作者单位： | 1. 海军驻景德镇地区航空军事代表室,江西景德镇,333000
2. 中国直升机设计研究所,江西景德镇,333001 |
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| 摘 要： | 建立了某型无人直升机的线性化模型,并对动态矩阵控制算法进行了相关的理论研究,结合经典的PID控制应用至某型无人直升机飞行控制系统控制律.经仿真验证,该设计方法可行、合理.
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| 关 键 词： | DMC PID 无人直升机 飞行控制 |
Design of The UMH Flight Control System Based on DMC-PID |
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| Authors: | SHAN Junjie DUAN Biao LAI Shuiqing |
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| Institution: | SHAN Junjie1,DUAN Biao2,LAI Shuiqing3 (1.Navy Aeronautic Representative Office to Jingdezhen,Jingdezhen 333000,China,2.China Helicopter Research and Development Institute,Jingdezhen 333001,China) |
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| Abstract: | The linear model of an unmanned helicopter (UMH) was built,and the Dynamic Matrix Control (DMC) algorithm was researched.Based on the above-mentioned work,the application about the predictive control with PID on the UMH flight control system was advanced.The simulations results demonstrate the algorithm was feasible. |
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| Keywords: | DMC PID unmanned helicopter flight control |
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