Relevant bibliographies by topics / Structured multimodel H¥ synthesis

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Book chapters
  4. Conference papers

Academic literature on the topic 'Structured multimodel H¥ synthesis'

Author: Grafiati
Published: 4 June 2021
Last updated: 8 February 2022

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Journal articles on the topic "Structured multimodel H¥ synthesis"

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Pensar, J. A., and H. T. Toivonen. "A Multimodel Mixed H 2 / H ∞ Problem for Plants with Structured Uncertainty." IFAC Proceedings Volumes 27, no. 2 (1994): 273–78. http://dx.doi.org/10.1016/s1474-6670(17)48163-8.

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Gahinet, P., and P. Apkarian. "Structured H∞ Synthesis in MATLAB." IFAC Proceedings Volumes 44, no. 1 (2011): 1435–40. http://dx.doi.org/10.3182/20110828-6-it-1002.00708.

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Ganet-Schoeller, M., and Jean Desmariaux. "Structured H∞ synthesis for flexible launcher control." IFAC-PapersOnLine 49, no. 17 (2016): 450–55. http://dx.doi.org/10.1016/j.ifacol.2016.09.077.

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Straßer, Marion, Joachim H. X. Schrauth, Sofia Dembski, et al. "Calcium fluoride based multifunctional nanoparticles for multimodal imaging." Beilstein Journal of Nanotechnology 8 (July 18, 2017): 1484–93. http://dx.doi.org/10.3762/bjnano.8.148.

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New multifunctional nanoparticles (NPs) that can be used as contrast agents (CA) in different imaging techniques, such as photoluminescence (PL) microscopy and magnetic resonance imaging (MRI), open new possibilities for medical imaging, e.g., in the fields of diagnostics or tissue characterization in regenerative medicine. The focus of this study is on the synthesis and characterization of CaF2:(Tb3+,Gd3+) NPs. Fabricated in a wet-chemical procedure, the spherical NPs with a diameter of 5–10 nm show a crystalline structure. Simultaneous doping of the NPs with different lanthanide ions, leadin
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Ma, Xiaochuan, Jie Yan, Wenxing Fu, and Kang Chen. "Autopilot Structured H∞ Synthesis for Satisfying Gain and Phase Margin Constraints." Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 37, no. 2 (2019): 211–17. http://dx.doi.org/10.1051/jnwpu/20193720211.

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Aiming at the static unstable Hypersonic vehicle, a method for designing H∞ autopilot to satisfy gain margin and phase margin is proposed. Structured H∞ synthesis is used to synthesize the autopilot under the fixed structure. The gain margin and phase margin were constrained by using H∞ norm of the complementary of the scaled plant. The requirement for the gain margin and phase margin is represented by the distance between the open loop Nyquist curve and the circle that represents the gain margin and phase margin in the complex plane. The distance is adjusted by tuning the parameter of perform
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Navarro-Tapia, D., P. Simplício, A. Iannelli, and A. Marcos. "Robust Flare Control Design Using Structured H ∞ Synthesis: a Civilian Aircraft Landing Challenge." IFAC-PapersOnLine 50, no. 1 (2017): 3971–76. http://dx.doi.org/10.1016/j.ifacol.2017.08.769.

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Keskin, Rıdvan, Ibrahim Aliskan, and Ersin Daş. "Robust structured controller synthesis for interleaved boost converters using an H∞ control method." Transactions of the Institute of Measurement and Control 43, no. 14 (2021): 3169–80. http://dx.doi.org/10.1177/01423312211019560.

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The regulation of output voltage and equivalent distribution of phase currents of multi-phase converters which have non-minimum phase characteristic are still challenges, especially in the presence of uncertainties in real parameters, duty cycle, input voltage, and load disturbances. However, in classical third-order integral-lead (Type-III) controller design methodologies, the controller is synthesized considering only the nominal performance conditions. This paper proposes a structured [Formula: see text] synthesis framework based on an optimization methodology to the design of a robust Type
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Arunkumar, Nagarajan. "Synthesis of Visible Light Active Delafossite Structured CuCrO2: Optical and Photocatalytic Studies." Asian Journal of Chemistry 33, no. 2 (2021): 465–70. http://dx.doi.org/10.14233/ajchem.2021.22932.

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Synthesis of delafossite structured CuCrO2 by sol-gel method using tartaric acid as a complexing agent is reported in present study. The product has been characterized by powder X-ray diffraction, thermal analysis (TGA/DTA), SEM, Raman spectra, BET (surface area analysis) and UV-Vis-diffused reflectance spectroscopy. Powder X-ray diffraction revealed the formation of delafossite structured CuCrO2 phase at 800 ºC for 3 h, which was further confirmed by thermal analysis that showed one weight loss and endothermic peak at above 800 ºC corresponded to the phase transition. Hexagonal plate like mor
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Tang, Jia-Ye, Cheng Zhan, Li-Xun Yang, Lu-Yuan Hao, Xin Xu, and Agathopoulos Simeon. "Synthesis of h-BN encapsulated spherical core–shell structured SiO2@Sr2Si5N8:Eu2+ red phosphors." Materials Chemistry and Physics 132, no. 2-3 (2012): 1089–94. http://dx.doi.org/10.1016/j.matchemphys.2011.12.073.

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Chen, Junyi, Baomin Feng, Zhengyong Guo, Bixuan Huang, Qifu Li, and Bei Lu. "Attitude dynamic tracking control of an agile satellite using a fixed-structured H∞ synthesis method." Aerospace Systems 3, no. 4 (2020): 243–53. http://dx.doi.org/10.1007/s42401-020-00066-7.

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Dissertations / Theses on the topic "Structured multimodel H¥ synthesis"

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Lesprier, Jérémy. "Synthèse et validation de lois de commande de vol robustes en présence d’incertitudes paramétriques et de non-linéarités." Thesis, Toulouse, ISAE, 2015. http://www.theses.fr/2015ESAE0031/document.

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Les méthodes de synthèse et de validation de lois de pilotage utiliséesdans le milieu industriel aéronautique sont bien souvent longues et coûteuses àmettre en œuvre. Pourtant, des alternatives pour traiter les larges domaine d’évolutionexistent, comme l’inversion dynamique robuste. Ce travail de thèse chercheà en corriger les défauts, notamment grâce à une meilleure prise en compte desincertitudes du système et à une réjection des non-linéarités non compensées. Ceciest rendu possible grâce aux techniques de synthèse H¥ structurée multi-modèles,qui peuvent considérer plusieurs configurations p
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Bibel, John Eugene. "Missile autopilot design using Mu-Synthesis." Thesis, This resource online, 1998. http://scholar.lib.vt.edu/theses/available/etd-08252008-161841/.

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Book chapters on the topic "Structured multimodel H¥ synthesis"

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Chambon, Emmanuel, Pierre Apkarian, and Laurent Burlion. "Flexible Launch Vehicle Control Using Robust Observer-Based Controller Obtained through Structured H ∞ Synthesis." In Advances in Aerospace Guidance, Navigation and Control. Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-17518-8_2.

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PENSAR, J. A., and H. T. TOIVONEN. "A MULTIMODEL MIXED H2 / H∞ PROBLEM FOR PLANTS WITH STRUCTURED UNCERTAINTY." In Advanced Control of Chemical Processes 1994. Elsevier, 1994. http://dx.doi.org/10.1016/b978-0-08-042229-9.50046-x.

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Conference papers on the topic "Structured multimodel H¥ synthesis"

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Saussie, David, Quentin Barbes, and Caroline Berard. "Self-scheduled and structured H⋡ synthesis : A launch vehicle application." In 2013 American Control Conference (ACC). IEEE, 2013. http://dx.doi.org/10.1109/acc.2013.6580062.

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Abroug, Neil, Xavier Lamy, and Edouard Laroche. "Human force augmentation: Optimal control parameters tuning using structured H∞ synthesis." In 2016 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS). IEEE, 2016. http://dx.doi.org/10.1109/iros.2016.7759129.

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Cai, Runze, Ruixiang Zheng, Ming Liu, and Mian Li. "Optimal selection of PI parameters of FOC for PMSM using structured H∞-synthesis." In IECON 2017 - 43rd Annual Conference of the IEEE Industrial Electronics Society. IEEE, 2017. http://dx.doi.org/10.1109/iecon.2017.8217511.

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Safonov, Michael. "Optimal H∞ synthesis of robust controllers for systems with structured uncertainty." In 1986 25th IEEE Conference on Decision and Control. IEEE, 1986. http://dx.doi.org/10.1109/cdc.1986.267276.

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Ho, Lok Man. "H∞ structured residual generator synthesis using residual reference models with application to lateral vehicle dynamics." In 2016 European Control Conference (ECC). IEEE, 2016. http://dx.doi.org/10.1109/ecc.2016.7810374.

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Nami, Chiramathe, Koichi Oka, and Akinori Harada. "H∞ structured controller synthesis applied to flight controller of QTW-UAV using meta-heuristic particle swarm optimization." In 2016 55th Annual Conference of the Society of Instrument and Control Engineers of Japan (SICE). IEEE, 2016. http://dx.doi.org/10.1109/sice.2016.7749271.

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Lefort, Alexandre, Xavier Dal Santo, Jordan Ninin, and Benoit Clement. "Depth Control of a Submarine: An Application of Structured H∞ Synthesis Method for Uncertain Models based on Interval Analysis." In 2018 Australian & New Zealand Control Conference (ANZCC). IEEE, 2018. http://dx.doi.org/10.1109/anzcc.2018.8606583.

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Watts, Stephen R., and Sanjay Garg. "A Comparison of Multivariable Control Design Techniques for a Turbofan Engine Control." In ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1995. http://dx.doi.org/10.1115/95-gt-258.

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This paper compares two previously published design procedures for two different multivariable control design techniques for application to a linear engine model of a jet engine. The two multivariable control design techniques compared were the Linear Quadratic Gaussian with Loop Transfer Recovery (LQG/LTR) and the H–Infinity (H∞) synthesis. The two control design techniques were used with specific previously published design procedures to synthesize controls which would provide equivalent closed loop frequency response for the primary control loops while assuring adequate loop de-coupling. Th
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Taylor, J. D., and William Messner. "Controller Design for Nonlinear Multi-Input/Multi-Output Systems Using the Contoured Robust Controller Bode Plot." In ASME 2013 Dynamic Systems and Control Conference. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/dscc2013-4047.

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In this paper, a novel approach to controller design for non-linear multi–input/multi–output (MIMO) systems is presented based on the Contoured Robust Controller Bode (CRCBode) plot. CRCBode plots show level–sets of a robust metric and identify certain “forbidden regions” on the controller Bode magnitude and phase plots such that intersections of the controller frequency response with these forbidden regions indicate that a robust stability and performance criterion is violated. Nonlinear system dynamics are included as a structured uncertainty set consisting of linearizations about several op
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