@inproceedings{ffe5a1ac704a4df7bf0e8e6b1511ea74,
title = "Limit cycle oscillation control of aeroelastic system using model-error control synthesis",
abstract = "Model-error control synthesis is a nonlinear robust control approach that uses an optimal solution to cancel the effects of modelling errors and external disturbances on a system. In this paper the optimal solution for a modified approximate receding-horizon problem is used to determine the model error in an aeroelastic system, which has several uncertain parameters, including a nonlinear spring constant. To verify the control performance the approach is applied to compensate the limit cycle oscillation of the system. Simulation results show the performance of the model-error control synthesis approach.",
author = "Jongrae Kim and Crassidis, \{John L.\}",
year = "2003",
doi = "10.2514/6.2003-5506",
language = "English",
isbn = "9781563479786",
series = "AIAA Guidance, Navigation, and Control Conference and Exhibit",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
booktitle = "AIAA Guidance, Navigation, and Control Conference and Exhibit",
note = "AIAA Guidance, Navigation, and Control Conference and Exhibit 2003 ; Conference date: 11-08-2003 Through 14-08-2003",
}