Sérgio R. Barros dos Santos, André M. de Oliveira, Oswaldo L. V. Costa, Gabriela W. Gabriel
{"title":"相位型半马尔可夫跳变线性系统的多目标控制在环内软件控制中的应用","authors":"Sérgio R. Barros dos Santos, André M. de Oliveira, Oswaldo L. V. Costa, Gabriela W. Gabriel","doi":"10.1002/rnc.8037","DOIUrl":null,"url":null,"abstract":"<div>\n \n <p>In this work, we tackle the multi-objective control for phase-type semi-Markov jump linear systems in the context of partial observation of the jump variable. Design conditions for state feedback controllers depending on cluster observations, which ensure bounds on the <span></span><math>\n <semantics>\n <mrow>\n <msub>\n <mrow>\n <mi>H</mi>\n </mrow>\n <mrow>\n <mn>2</mn>\n </mrow>\n </msub>\n </mrow>\n <annotation>$$ {H}_2 $$</annotation>\n </semantics></math>, <span></span><math>\n <semantics>\n <mrow>\n <msub>\n <mrow>\n <mi>H</mi>\n </mrow>\n <mrow>\n <mi>∞</mi>\n </mrow>\n </msub>\n </mrow>\n <annotation>$$ {H}_{\\infty } $$</annotation>\n </semantics></math>, and energy-to-peak performance indices, are given in terms of linear matrix inequalities. The robust case in which the system matrices are uncertain and described by suitable polytopes is also considered. By restricting to the pure Markov jump linear system case with perfect observation of the Markov chain, we show that the <span></span><math>\n <semantics>\n <mrow>\n <msub>\n <mrow>\n <mi>H</mi>\n </mrow>\n <mrow>\n <mn>2</mn>\n </mrow>\n </msub>\n </mrow>\n <annotation>$$ {H}_2 $$</annotation>\n </semantics></math> and <span></span><math>\n <semantics>\n <mrow>\n <msub>\n <mrow>\n <mi>H</mi>\n </mrow>\n <mrow>\n <mi>∞</mi>\n </mrow>\n </msub>\n </mrow>\n <annotation>$$ {H}_{\\infty } $$</annotation>\n </semantics></math> conditions yield the optimal controllers when solved separately. For validating the results, two types of simulation for controlling an aircraft subject to faults are presented, namely, a conventional <i>Model-in-the-Loop</i> setting, in which the controller and the plant are simulated in the same scientific software; and a <i>Software-in-the-Loop</i> simulation, in which a realistic flight simulator is employed. The simulation results illustrate the effectiveness of the proposed method and are close to the theoretical predictions, suggesting a powerful tool for validating semi-Markov jump controllers in practical settings.</p>\n </div>","PeriodicalId":50291,"journal":{"name":"International Journal of Robust and Nonlinear Control","volume":"35 14","pages":"6071-6090"},"PeriodicalIF":3.2000,"publicationDate":"2025-05-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Multi-Objective Control of Phase-Type Semi-Markov Jump Linear Systems Applied to Software-In-The-Loop Aircraft Control\",\"authors\":\"Sérgio R. Barros dos Santos, André M. de Oliveira, Oswaldo L. V. Costa, Gabriela W. Gabriel\",\"doi\":\"10.1002/rnc.8037\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div>\\n \\n <p>In this work, we tackle the multi-objective control for phase-type semi-Markov jump linear systems in the context of partial observation of the jump variable. Design conditions for state feedback controllers depending on cluster observations, which ensure bounds on the <span></span><math>\\n <semantics>\\n <mrow>\\n <msub>\\n <mrow>\\n <mi>H</mi>\\n </mrow>\\n <mrow>\\n <mn>2</mn>\\n </mrow>\\n </msub>\\n </mrow>\\n <annotation>$$ {H}_2 $$</annotation>\\n </semantics></math>, <span></span><math>\\n <semantics>\\n <mrow>\\n <msub>\\n <mrow>\\n <mi>H</mi>\\n </mrow>\\n <mrow>\\n <mi>∞</mi>\\n </mrow>\\n </msub>\\n </mrow>\\n <annotation>$$ {H}_{\\\\infty } $$</annotation>\\n </semantics></math>, and energy-to-peak performance indices, are given in terms of linear matrix inequalities. The robust case in which the system matrices are uncertain and described by suitable polytopes is also considered. By restricting to the pure Markov jump linear system case with perfect observation of the Markov chain, we show that the <span></span><math>\\n <semantics>\\n <mrow>\\n <msub>\\n <mrow>\\n <mi>H</mi>\\n </mrow>\\n <mrow>\\n <mn>2</mn>\\n </mrow>\\n </msub>\\n </mrow>\\n <annotation>$$ {H}_2 $$</annotation>\\n </semantics></math> and <span></span><math>\\n <semantics>\\n <mrow>\\n <msub>\\n <mrow>\\n <mi>H</mi>\\n </mrow>\\n <mrow>\\n <mi>∞</mi>\\n </mrow>\\n </msub>\\n </mrow>\\n <annotation>$$ {H}_{\\\\infty } $$</annotation>\\n </semantics></math> conditions yield the optimal controllers when solved separately. For validating the results, two types of simulation for controlling an aircraft subject to faults are presented, namely, a conventional <i>Model-in-the-Loop</i> setting, in which the controller and the plant are simulated in the same scientific software; and a <i>Software-in-the-Loop</i> simulation, in which a realistic flight simulator is employed. The simulation results illustrate the effectiveness of the proposed method and are close to the theoretical predictions, suggesting a powerful tool for validating semi-Markov jump controllers in practical settings.</p>\\n </div>\",\"PeriodicalId\":50291,\"journal\":{\"name\":\"International Journal of Robust and Nonlinear Control\",\"volume\":\"35 14\",\"pages\":\"6071-6090\"},\"PeriodicalIF\":3.2000,\"publicationDate\":\"2025-05-15\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"International Journal of Robust and Nonlinear Control\",\"FirstCategoryId\":\"94\",\"ListUrlMain\":\"https://onlinelibrary.wiley.com/doi/10.1002/rnc.8037\",\"RegionNum\":3,\"RegionCategory\":\"计算机科学\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q2\",\"JCRName\":\"AUTOMATION & CONTROL SYSTEMS\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"International Journal of Robust and Nonlinear Control","FirstCategoryId":"94","ListUrlMain":"https://onlinelibrary.wiley.com/doi/10.1002/rnc.8037","RegionNum":3,"RegionCategory":"计算机科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"AUTOMATION & CONTROL SYSTEMS","Score":null,"Total":0}
Multi-Objective Control of Phase-Type Semi-Markov Jump Linear Systems Applied to Software-In-The-Loop Aircraft Control
In this work, we tackle the multi-objective control for phase-type semi-Markov jump linear systems in the context of partial observation of the jump variable. Design conditions for state feedback controllers depending on cluster observations, which ensure bounds on the , , and energy-to-peak performance indices, are given in terms of linear matrix inequalities. The robust case in which the system matrices are uncertain and described by suitable polytopes is also considered. By restricting to the pure Markov jump linear system case with perfect observation of the Markov chain, we show that the and conditions yield the optimal controllers when solved separately. For validating the results, two types of simulation for controlling an aircraft subject to faults are presented, namely, a conventional Model-in-the-Loop setting, in which the controller and the plant are simulated in the same scientific software; and a Software-in-the-Loop simulation, in which a realistic flight simulator is employed. The simulation results illustrate the effectiveness of the proposed method and are close to the theoretical predictions, suggesting a powerful tool for validating semi-Markov jump controllers in practical settings.
期刊介绍:
Papers that do not include an element of robust or nonlinear control and estimation theory will not be considered by the journal, and all papers will be expected to include significant novel content. The focus of the journal is on model based control design approaches rather than heuristic or rule based methods. Papers on neural networks will have to be of exceptional novelty to be considered for the journal.