| 复合式高速直升机过渡模式控制器设计 |
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| 引用本文： | 江顺,陈燕云,何伟,盛守照.复合式高速直升机过渡模式控制器设计[J].机械制造与自动化,2021,50(1):184-187,219. |
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| 作者姓名： | 江顺 陈燕云 何伟 盛守照 |
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| 作者单位： | 南京航空航天大学 自动化学院,江苏 南京210016;南京航空航天大学 自动化学院,江苏 南京210016;南京航空航天大学 自动化学院,江苏 南京210016;南京航空航天大学 自动化学院,江苏 南京210016 |
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| 基金项目： | 国防重大项目培育基金项目 |
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| 摘 要： | 以复合式高速直升机为研究对象,建立整机气动模型。针对复合式高速直升机过渡模式中存在强非线性、控制输入转移的问题,提出一种基于操稳性和推进功率最优的控制分配方法,设计过渡模式自适应PID控制器,进行仿真验证。仿真结果表明:该控制器可以有效保证复合式高速直升机过渡模式的安全性和平稳性。
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| 关 键 词： | 复合式高速直升机 过渡模式 控制分配 控制器设计 |
Controller Design for Compound High-speed Helicopter Under Transition Mode |
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| JIANG Shun,CHEN Yanyun,HE Wei,SHENG Shouzhao.Controller Design for Compound High-speed Helicopter Under Transition Mode[J].Machine Building & Automation,2021,50(1):184-187,219. |
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| Authors: | JIANG Shun CHEN Yanyun HE Wei SHENG Shouzhao |
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| Affiliation: | (College of Automation Engineering,Nanjing University of Aeronautic and Astronautics,Nanjing 210016,China) |
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| Abstract: | Taken the compound high-speed helicopter as the research object,the aerodynamic models of the whole helicopter is established.As to the problem of strong nonlinearity and control input transfer in the transition mode of compound high-speed helicopter,a control allocation method based on the optimal operation stability and propulsion power is proposedintially.Then a transition mode adaptive PID controller is designed,and simulation verification is undertaken in the end.The simulati on results show that the controller is effectively in guaranteeing the safety and stability of the transition mode of the compound high-speed helicopter. |
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| Keywords: | compound high-speed helicopter transition mode control allocation controller design |
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