带扰动的直升机恒加比例趋近律跟踪控制

2016 International Conference on Micro-Electronics and Telecommunication Engineering (ICMETE) Pub Date : 2016-09-01 DOI:10.1109/ICMETE.2016.38

Puja Yadav, Rajshree Taparia

{"title":"带扰动的直升机恒加比例趋近律跟踪控制","authors":"Puja Yadav, Rajshree Taparia","doi":"10.1109/ICMETE.2016.38","DOIUrl":null,"url":null,"abstract":"This paper describes the tracking of flight height andpitch angle of a helicopter model using output feedbackcontroller. A sliding mode control (SMC) methodology based onfeedback linearization and constant plus proportional reachinglaw is used. The sliding mode control method is robust withdisturbances. The mathematical model of helicopter is simplifiedby using dynamic inversion uncoupling linearization. The controllaw based on reaching law is designed to achieve the desiredobjectives. The tracking performance demonstrated insimulation results.","PeriodicalId":167368,"journal":{"name":"2016 International Conference on Micro-Electronics and Telecommunication Engineering (ICMETE)","volume":"13 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2016-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Tracking Control of Helicopter Using Constant Plus Proportional Reaching Law with Disturbances\",\"authors\":\"Puja Yadav, Rajshree Taparia\",\"doi\":\"10.1109/ICMETE.2016.38\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper describes the tracking of flight height andpitch angle of a helicopter model using output feedbackcontroller. A sliding mode control (SMC) methodology based onfeedback linearization and constant plus proportional reachinglaw is used. The sliding mode control method is robust withdisturbances. The mathematical model of helicopter is simplifiedby using dynamic inversion uncoupling linearization. The controllaw based on reaching law is designed to achieve the desiredobjectives. The tracking performance demonstrated insimulation results.\",\"PeriodicalId\":167368,\"journal\":{\"name\":\"2016 International Conference on Micro-Electronics and Telecommunication Engineering (ICMETE)\",\"volume\":\"13 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2016-09-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2016 International Conference on Micro-Electronics and Telecommunication Engineering (ICMETE)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICMETE.2016.38\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2016 International Conference on Micro-Electronics and Telecommunication Engineering (ICMETE)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICMETE.2016.38","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}

引用次数: 0

摘要

本文介绍了利用输出反馈控制器对直升机模型的飞行高度和俯仰角进行跟踪的方法。采用了一种基于反馈线性化和常数加比例达到律的滑模控制方法。滑模控制方法对干扰具有鲁棒性。采用动态反演解耦线性化方法简化了直升机的数学模型。基于趋近律的控制律设计是为了实现预期目标。仿真结果验证了跟踪性能。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

查看原文本刊更多论文

Tracking Control of Helicopter Using Constant Plus Proportional Reaching Law with Disturbances

This paper describes the tracking of flight height andpitch angle of a helicopter model using output feedbackcontroller. A sliding mode control (SMC) methodology based onfeedback linearization and constant plus proportional reachinglaw is used. The sliding mode control method is robust withdisturbances. The mathematical model of helicopter is simplifiedby using dynamic inversion uncoupling linearization. The controllaw based on reaching law is designed to achieve the desiredobjectives. The tracking performance demonstrated insimulation results.

求助全文

通过发布文献求助，成功后即可免费获取论文全文。去求助

来源期刊

2016 International Conference on Micro-Electronics and Telecommunication Engineering (ICMETE)

自引率

0.00%

发文量