{"title":"吸气式高超声速飞行器状态反馈PID控制设计","authors":"Rites Singh, O. Prakash, S. Joshi","doi":"10.5937/fme2302221s","DOIUrl":null,"url":null,"abstract":"The paper uses the state feedback technique to provide a control design method for a dynamic linear 6-degree-of-freedom (DOF) model of an Airbreathing Hypersonic Vehicle (AHV). A linear model of AHV with a state space model is developed for the open loop simulation for the level flight with Mach number 5 and a height of 65000 ft (19812 m). The dynamic stability of AHV is analyzed, and state feedback with the pole placement method is implemented for the controller design. The dynamic stability, response, and comparison for the PI and PID controller are presented for the aileron deflection da and rudder deflection dr for the AHV linear model.","PeriodicalId":12218,"journal":{"name":"FME Transactions","volume":null,"pages":null},"PeriodicalIF":1.2000,"publicationDate":"2023-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Control design using PID with state feedback for Air-breathing Hypersonic Vehicle\",\"authors\":\"Rites Singh, O. Prakash, S. Joshi\",\"doi\":\"10.5937/fme2302221s\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The paper uses the state feedback technique to provide a control design method for a dynamic linear 6-degree-of-freedom (DOF) model of an Airbreathing Hypersonic Vehicle (AHV). A linear model of AHV with a state space model is developed for the open loop simulation for the level flight with Mach number 5 and a height of 65000 ft (19812 m). The dynamic stability of AHV is analyzed, and state feedback with the pole placement method is implemented for the controller design. The dynamic stability, response, and comparison for the PI and PID controller are presented for the aileron deflection da and rudder deflection dr for the AHV linear model.\",\"PeriodicalId\":12218,\"journal\":{\"name\":\"FME Transactions\",\"volume\":null,\"pages\":null},\"PeriodicalIF\":1.2000,\"publicationDate\":\"2023-01-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"FME Transactions\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.5937/fme2302221s\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q3\",\"JCRName\":\"ENGINEERING, MECHANICAL\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"FME Transactions","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.5937/fme2302221s","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"ENGINEERING, MECHANICAL","Score":null,"Total":0}
引用次数: 0
摘要
采用状态反馈技术，为吸气式高超声速飞行器(AHV)的动态线性6自由度模型提供了一种控制设计方法。针对马赫数为5、高度为65000 ft (19812 m)的水平飞行，建立了一种具有状态空间模型的AHV线性模型，分析了AHV的动态稳定性，采用极点放置法进行状态反馈，设计了AHV控制器。对AHV线性模型的副翼偏转数据和方向舵偏转dr进行了动态稳定性、响应性和PI控制器与PID控制器的比较。
Control design using PID with state feedback for Air-breathing Hypersonic Vehicle
The paper uses the state feedback technique to provide a control design method for a dynamic linear 6-degree-of-freedom (DOF) model of an Airbreathing Hypersonic Vehicle (AHV). A linear model of AHV with a state space model is developed for the open loop simulation for the level flight with Mach number 5 and a height of 65000 ft (19812 m). The dynamic stability of AHV is analyzed, and state feedback with the pole placement method is implemented for the controller design. The dynamic stability, response, and comparison for the PI and PID controller are presented for the aileron deflection da and rudder deflection dr for the AHV linear model.
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