{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2026,5,4]],"date-time":"2026-05-04T16:10:10Z","timestamp":1777911010338,"version":"3.51.4"},"reference-count":43,"publisher":"SAGE Publications","issue":"2","license":[{"start":{"date-parts":[[2025,1,17]],"date-time":"2025-01-17T00:00:00Z","timestamp":1737072000000},"content-version":"tdm","delay-in-days":0,"URL":"https:\/\/journals.sagepub.com\/page\/policies\/text-and-data-mining-license"}],"funder":[{"name":"1912 Project"},{"name":"the Chinese Aviation Science Foundation","award":["20220058068001"],"award-info":[{"award-number":["20220058068001"]}]}],"content-domain":{"domain":["journals.sagepub.com"],"crossmark-restriction":true},"short-container-title":["Transactions of the Institute of Measurement and Control"],"published-print":{"date-parts":[[2026,1]]},"abstract":"<jats:p>\n                    This article investigates the problem of finite-time control for the mode transition of turbine-based combined cycle (TBCC) engines described in the polynomial parameter-varying (PPV) framework. In order to realize small-deviation mode transition, a PPV model that can be applied to different opening rates of an inlet splitter is established for a TBCC project put forward by Xiamen University named Xiamen Turbine-based Ejector Ramjet (XTER). The concepts of\n                    <jats:inline-formula>\n                      <mml:math xmlns:mml=\"http:\/\/www.w3.org\/1998\/Math\/MathML\" display=\"inline\" overflow=\"scroll\">\n                        <mml:mrow>\n                          <mml:msub>\n                            <mml:mrow>\n                              <mml:mi>H<\/mml:mi>\n                            <\/mml:mrow>\n                            <mml:mrow>\n                              <mml:mi>\u221e<\/mml:mi>\n                            <\/mml:mrow>\n                          <\/mml:msub>\n                        <\/mml:mrow>\n                      <\/mml:math>\n                    <\/jats:inline-formula>\n                    uniformly finite-time stability and\n                    <jats:inline-formula>\n                      <mml:math xmlns:mml=\"http:\/\/www.w3.org\/1998\/Math\/MathML\" display=\"inline\" overflow=\"scroll\">\n                        <mml:mrow>\n                          <mml:msub>\n                            <mml:mrow>\n                              <mml:mi>H<\/mml:mi>\n                            <\/mml:mrow>\n                            <mml:mrow>\n                              <mml:mi>\u221e<\/mml:mi>\n                            <\/mml:mrow>\n                          <\/mml:msub>\n                        <\/mml:mrow>\n                      <\/mml:math>\n                    <\/jats:inline-formula>\n                    uniformly finite-time output tracking performance are proposed, together with the corresponding state-and-parameter-dependent controller design conditions which can be efficiently solved by using sum-of-squares programming. Meanwhile, based on the PPV system of XTER, the controllers are designed in the designed flight conditions and the non-designed flight conditions, respectively. Finally, simulation results on the mode transition of the XTER are given to verify the feasibility and effectiveness of the proposed control scheme.\n                  <\/jats:p>","DOI":"10.1177\/01423312241300745","type":"journal-article","created":{"date-parts":[[2025,1,18]],"date-time":"2025-01-18T00:54:13Z","timestamp":1737161653000},"page":"311-322","update-policy":"https:\/\/doi.org\/10.1177\/sage-journals-update-policy","source":"Crossref","is-referenced-by-count":0,"title":["Finite-time control for polynomial parameter-varying systems and its application in mode transition of turbine-based combined cycle engines"],"prefix":"10.1177","volume":"48","author":[{"ORCID":"https:\/\/orcid.org\/0009-0000-9640-0639","authenticated-orcid":false,"given":"Lianchen","family":"Yu","sequence":"first","affiliation":[{"name":"School of Aerospace Engineering, Xiamen University, Xiamen, Fujian, China"}]},{"given":"Chenlong","family":"Yang","sequence":"additional","affiliation":[{"name":"School of Aerospace Engineering, Xiamen University, Xiamen, Fujian, China"}]},{"given":"Hongfei","family":"Sun","sequence":"additional","affiliation":[{"name":"School of Aerospace Engineering, Xiamen University, Xiamen, Fujian, China"}]},{"ORCID":"https:\/\/orcid.org\/0000-0002-3811-6557","authenticated-orcid":false,"given":"Jianping","family":"Zeng","sequence":"additional","affiliation":[{"name":"School of Aerospace Engineering, Xiamen University, Xiamen, Fujian, China"}]}],"member":"179","published-online":{"date-parts":[[2025,1,17]]},"reference":[{"key":"e_1_3_3_2_1","doi-asserted-by":"publisher","DOI":"10.1109\/TAC.2010.2041680"},{"key":"e_1_3_3_3_1","doi-asserted-by":"publisher","DOI":"10.1016\/j.automatica.2019.06.002"},{"key":"e_1_3_3_4_1","doi-asserted-by":"publisher","DOI":"10.1137\/S0363012997321358"},{"key":"e_1_3_3_5_1","doi-asserted-by":"publisher","DOI":"10.1002\/rnc.3399"},{"key":"e_1_3_3_6_1","doi-asserted-by":"publisher","DOI":"10.1016\/S1000-9361(08)60130-2"},{"key":"e_1_3_3_7_1","doi-asserted-by":"publisher","DOI":"10.1109\/TAC.2011.2159419"},{"key":"e_1_3_3_8_1","doi-asserted-by":"publisher","DOI":"10.1002\/rnc.4304"},{"key":"e_1_3_3_9_1","doi-asserted-by":"publisher","DOI":"10.1080\/00207179.2018.1442022"},{"key":"e_1_3_3_10_1","first-page":"171","article-title":"Modeling and mode transition simulation of over-under turbine based combined cycle (TBCC) propulsion system based on inlet\/engine matching","volume":"40","author":"Gao Y","year":"2023","unstructured":"Gao Y, Xi ZH, Hu CX, et al. 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