Uros Kalabic, I. Kolmanovsky, J. Buckland, E. Gilbert
{"title":"基于线性模型的涡轮增压汽油机控制参考和扩展命令调速器","authors":"Uros Kalabic, I. Kolmanovsky, J. Buckland, E. Gilbert","doi":"10.1109/CCA.2011.6044457","DOIUrl":null,"url":null,"abstract":"In this paper, reference and extended command governors are developed for enforcing constraints in the air path of turbo-charged gasoline engines. These governors are add-on control schemes which protect the engine from violating pointwise-in-time state and control constraints, including compressor surge and actuator limits. Several design choices based on linear engine models at different operating points are compared in terms of response speed, sets of recoverable initial conditions, tolerance of disturbances, and computational complexity. The final design is implemented on the nonlinear engine model. Further, an approach to handle intake manifold pressure overshoot constraints, and a novel form of the extended command governor based on Laguerre's sequences are presented.","PeriodicalId":208713,"journal":{"name":"2011 IEEE International Conference on Control Applications (CCA)","volume":"70 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2011-10-13","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"44","resultStr":"{\"title\":\"Reference and extended command governors for control of turbocharged gasoline engines based on linear models\",\"authors\":\"Uros Kalabic, I. Kolmanovsky, J. Buckland, E. Gilbert\",\"doi\":\"10.1109/CCA.2011.6044457\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In this paper, reference and extended command governors are developed for enforcing constraints in the air path of turbo-charged gasoline engines. These governors are add-on control schemes which protect the engine from violating pointwise-in-time state and control constraints, including compressor surge and actuator limits. Several design choices based on linear engine models at different operating points are compared in terms of response speed, sets of recoverable initial conditions, tolerance of disturbances, and computational complexity. The final design is implemented on the nonlinear engine model. Further, an approach to handle intake manifold pressure overshoot constraints, and a novel form of the extended command governor based on Laguerre's sequences are presented.\",\"PeriodicalId\":208713,\"journal\":{\"name\":\"2011 IEEE International Conference on Control Applications (CCA)\",\"volume\":\"70 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2011-10-13\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"44\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2011 IEEE International Conference on Control Applications (CCA)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/CCA.2011.6044457\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2011 IEEE International Conference on Control Applications (CCA)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/CCA.2011.6044457","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Reference and extended command governors for control of turbocharged gasoline engines based on linear models
In this paper, reference and extended command governors are developed for enforcing constraints in the air path of turbo-charged gasoline engines. These governors are add-on control schemes which protect the engine from violating pointwise-in-time state and control constraints, including compressor surge and actuator limits. Several design choices based on linear engine models at different operating points are compared in terms of response speed, sets of recoverable initial conditions, tolerance of disturbances, and computational complexity. The final design is implemented on the nonlinear engine model. Further, an approach to handle intake manifold pressure overshoot constraints, and a novel form of the extended command governor based on Laguerre's sequences are presented.