ADAPTIVE CONTROL OF PITCH ANGLE FOR LAAS 'HELICOPTER' BENCHMARK

机译：LAAS“直升机”基准的俯仰角的自适应控制

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Based on the Speed-Gradient (SG) design method and the "Implicit Reference Model" (IRM) concept, two adaptive control laws for pitch angle control of the Quanser/LAAS "Helicopter" benchmark laboratory setup are designed and experimentally tested. The MATLAB/Simulink and WinCon software environment is used for adaptive control laws implementation and the real-world experiments. The experimental results demonstrate high closed loop system performance and robustness of the suggested control laws with respect to parametric uncertainties and unmodeled plant dynamics.

机译：基于速度梯度（SG）设计方法和“隐式参考模型”（IRM）概念，设计并通过实验测试了两种用于Quanser / LAAS“直升机”基准实验室设置的俯仰角控制的自适应控制律。 MATLAB / Simulink和WinCon软件环境用于自适应控制法则的实现和实际实验。实验结果表明，对于参数不确定性和未建模的工厂动态，高闭环系统性能和建议控制律的鲁棒性。

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来源
《Saint Petersburg International Conference on Integrated Navigation Systems; 20050523-25; Saint Petersburg(RU)》|2005年|P.33-39|共7页
会议地点 Saint Petersburg(RU)
作者
B.R. Andrievsky; D. Arzelier; A.L. Fradkov; D. Peaucelle;
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作者单位

CCS Lab., Institute for Problems of Mechanical Engineering of RAS 61, Bolshoy Ave., V.O., 199178, Saint Petersburg, Russia;

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原文格式 PDF
正文语种 eng
中图分类导航设备;
关键词
adaptive control; helicopter benchmark; autopilot design; experimental results;

机译：自适应控制;直升机基准;自动驾驶仪设计;实验结果;

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1. Discussion on: 'Adaptive Control Design and Experiments for LAAS 'Helicopter' Benchmark' [J] . R. Lozano, J.A. Escareno European Journal of Control . 2008,第4期

机译：讨论：“ LAAS“直升机”基准的自适应控制设计和实验”
2. Adaptive Control Design and Experiments for LAAS 'Helicopter' Benchmark [J] . A.L. Fradkov, B. Andrievsky, D. Peaucelle European Journal of Control . 2008,第4期

机译：LAAS“直升机”基准测试的自适应控制设计和实验
3. Adaptive Control of Helicopter Pitch Angle and Velocity [J] . Romulus Lungu, Mihai Lungu Journal of aerospace engineering . 2014,第5期

机译：直升机俯仰角和速度的自适应控制
4. ADAPTIVE CONTROL OF PITCH ANGLE FOR LAAS 'HELICOPTER' BENCHMARK [C] . B.R. Andrievsky, D. Arzelier, A.L. Fradkov, Saint Petersburg International Conference on Integrated Navigation Systems . 2005

机译：LAAS'直升机'基准的俯仰角度自适应控制
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ADAPTIVE CONTROL OF PITCH ANGLE FOR LAAS 'HELICOPTER' BENCHMARK

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