Zobrazeno 1 - 6
of 6
pro vyhledávání: '"S. H. Rajani"'
Publikováno v:
Automatic Control and Computer Sciences. 51:399-409
Hypersonic wind tunnel is a ground-based facility used to study the aerodynamic properties of space vehicles during re-entry. This paper aims at designing an H-infinity controller with krill herd optimization algorithm to regulate pressure inside the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3ae83a1b6b2ee32ba3eb3e0ae71640c2
https://doi.org/10.3103/s0146411617060074
https://doi.org/10.3103/s0146411617060074
Autor:
Bindu M. Krishna, S. H. Rajani
Publikováno v:
2017 International Conference on Innovative Mechanisms for Industry Applications (ICIMIA).
Hypersonic wind tunnels are used to study the performance of space vehicles inside the test specimen under hypersonic flow conditions. This paper aims at designing a chatter free sliding mode controller for regulation of pressure inside the settling
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::03307276bbc727351586a88a57a55ceb
https://doi.org/10.1109/icimia.2017.7975636
https://doi.org/10.1109/icimia.2017.7975636
Publikováno v:
International Journal of Modelling, Identification and Control. 29:78
Hypersonic wind tunnels are used for investigating the aerodynamic properties of vehicles during re-entry missions. This paper aims at designing a model reference adaptive control (MRAC) and modified adaptive control (MAC) for regulation of pressure
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::00539bde302f5af8355e082de0514a3b
https://doi.org/10.1504/ijmic.2018.089625
https://doi.org/10.1504/ijmic.2018.089625
Publikováno v:
Proceedings of the International Conference on Emerging Trends in Engineering & Technology (ICETET-2015).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::52703b78025371b953400e7fa363af83
https://doi.org/10.3850/978-981-09-5346-1_cse-538
https://doi.org/10.3850/978-981-09-5346-1_cse-538
Autor:
Usha Nair, S. H. Rajani
Publikováno v:
2013 IEEE International Conference on Computational Intelligence and Computing Research.
Hypersonic wind tunnel system facilitates the study of aerodynamic forces on space vehicles by passing a stream of velocity controlled air over them. In the present work, a backstepping controller for the settling chamber pressure of a continuous hyp
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8f62464a44c93b3b3c1c4a3181ba269b
https://doi.org/10.1109/iccic.2013.6724138
https://doi.org/10.1109/iccic.2013.6724138
Publikováno v:
2012 IEEE International Conference on Computational Intelligence and Computing Research.
This paper presents the effect of temperature inside the settling chamber of a hypersonic wind tunnel which is a test facility used to study the effect of aerodynamic forces on the specimen under test. Regulation of pressure inside the settling chamb
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a984fa00cfd0286d6e29fa6855709414
https://doi.org/10.1109/iccic.2012.6510283
https://doi.org/10.1109/iccic.2012.6510283