| タイトル | Parameter Estimation of Actuators for Benchmark Active Control Technology (BACT) Wind Tunnel Model with Analysis of Wear and Aerodynamic Loading Effects |
| 本文（外部サイト） | http://hdl.handle.net/2060/19980211327 |
| 著者（英） | Fung, Jimmy; Waszak, Martin R. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1998-07-01 |
| 言語 | eng |
| 内容記述 | This report describes the development of transfer function models for the trailing-edge and upper and lower spoiler actuators of the Benchmark Active Control Technology (BACT) wind tunnel model for application to control system analysis and design. A simple nonlinear least-squares parameter estimation approach is applied to determine transfer function parameters from frequency response data. Unconstrained quasi-Newton minimization of weighted frequency response error was employed to estimate the transfer function parameters. An analysis of the behavior of the actuators over time to assess the effects of wear and aerodynamic load by using the transfer function models is also presented. The frequency responses indicate consistent actuator behavior throughout the wind tunnel test and only slight degradation in effectiveness due to aerodynamic hinge loading. The resulting actuator models have been used in design, analysis, and simulation of controllers for the BACT to successfully suppress flutter over a wide range of conditions. |
| NASA分類 | Aircraft Stability and Control |
| レポートNO | AIAA Paper 96-3362
L-17540
NASA/TM-1998-208452
NAS 1.15:208452 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/98549 |
