| タイトル | Analytical and Experimental Evaluation of Digital Control Systems for the Semi-Span Super-Sonic Transport (S4T) Wind Tunnel Model |
| 本文（外部サイト） | http://hdl.handle.net/2060/20120008165 |
| 著者（英） | Christhilf, David; Perry, Boyd, III; Wieseman, Carol D. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2012-04-23 |
| 言語 | eng |
| 内容記述 | An important objective of the Semi-Span Super-Sonic Transport (S4T) wind tunnel model program was the demonstration of Flutter Suppression (FS), Gust Load Alleviation (GLA), and Ride Quality Enhancement (RQE). It was critical to evaluate the stability and robustness of these control laws analytically before testing them and experimentally while testing them to ensure safety of the model and the wind tunnel. MATLAB based software was applied to evaluate the performance of closed-loop systems in terms of stability and robustness. Existing software tools were extended to use analytical representations of the S4T and the control laws to analyze and evaluate the control laws prior to testing. Lessons were learned about the complex windtunnel model and experimental testing. The open-loop flutter boundary was determined from the closed-loop systems. A MATLAB/Simulink Simulation developed under the program is available for future work to improve the CPE process. This paper is one of a series of that comprise a special session, which summarizes the S4T wind-tunnel program. |
| NASA分類 | Aerodynamics |
| レポートNO | AIAA Paper 2012-1554
NF1676L-13302 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
