Iterative Learning Control of a Nonlinear Aeroelastic System with Parametric uncertainties
Author:
Affiliation:
1. School of mechanical and control engineering, Guilin University of Technology, Guilin, China
Funder
Research Foundation of Guilin University of Technology
Publisher
ACM
Link
https://dl.acm.org/doi/pdf/10.1145/3436286.3436745
Reference15 articles.
1. Lee I Kim S H. Aeroelastic analysis of a flexible control surface with structural nonlinearity[J]. journal of Aircraft 1995 32(4): 868--874. DOI: https://doi.org/10.2514/3.46803 Lee I Kim S H. Aeroelastic analysis of a flexible control surface with structural nonlinearity[J]. journal of Aircraft 1995 32(4): 868--874. DOI: https://doi.org/10.2514/3.46803
2. Ko J Kurdila A J Strganac T W. Nonlinear control of a prototypical wing section with torsional nonlinearity[J]. Journal of Guidance Control and Dynamics 1997 20(6): 1181--1189. DOI: https://doi.org/10.2514/2.4174 Ko J Kurdila A J Strganac T W. Nonlinear control of a prototypical wing section with torsional nonlinearity[J]. Journal of Guidance Control and Dynamics 1997 20(6): 1181--1189. DOI: https://doi.org/10.2514/2.4174
3. Tadi M. State-dependent Riccati equation for control of aeroelastic flutter[J]. Journal of guidance control and dynamics 2003 26(6): 914--917. DOI: https://doi.org/10.2514/2.6918 Tadi M. State-dependent Riccati equation for control of aeroelastic flutter[J]. Journal of guidance control and dynamics 2003 26(6): 914--917. DOI: https://doi.org/10.2514/2.6918
4. Bhoir N Singh S N. Control of unsteady aeroelastic system via state-dependent Riccati equation method[J]. Journal of Guidance Control and Dynamics 2005 28(1): 78--84. DOI: https://doi.org/10.2514/1.6590 Bhoir N Singh S N. Control of unsteady aeroelastic system via state-dependent Riccati equation method[J]. Journal of Guidance Control and Dynamics 2005 28(1): 78--84. DOI: https://doi.org/10.2514/1.6590
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