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- W2320113805 abstract "A framework for aeroservoelastic computations of a typical business jet conguration is presented. The eects of a nonlinear actuator model on control surface stability under various actuator failure scenarios are examined. The various failures result in the actuator dynamics becoming highly nonlinear in both amplitude and frequency. Unsteady Generalized Aerodynamic Force (GAF) matrices are obtained from MSC/Nastran at various Mach numbers and reduced frequencies. The GAF’s and the structural modal data are then used in ZAERO to generate state-space models of the aeroelastic system comprising the complete aircraft conguration at various ight conditions. These state-space models are then coupled with a nonlinear actuator model in the Matlab/Simulink environment. Free-play in the actuator and its linkages can also be simulated with this framework. The response of the control surface to various initial conditions is examined in the presence of free-play and/or the nonlinear actuator, including the variation of internal actuator parameters subject to normal production tolerance ranges. Limit Cycle Oscillations (LCO) are observed at various ight conditions. The paper highlights some important considerations in aeroservoelastic modeling and simulation of a typical business jet conguration involving actuator nonlinearities." @default.
- W2320113805 created "2016-06-24" @default.
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- W2320113805 date "2010-06-14" @default.
- W2320113805 modified "2023-09-25" @default.
- W2320113805 title "Aeroservoelastic Analysis of a Typical Business Jet Configuration Involving Nonlinear Actuators" @default.
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- W2320113805 doi "https://doi.org/10.2514/6.2010-8114" @default.
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