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Development of a Forced Oscillation System for Measuring Dynamic Derivatives of Fluidic VehiclesA new Forced Oscillation System (FOS) has been designed and built at NASA Langley Research Center that provides new capabilities for aerodynamic researchers to investigate the dynamic derivatives of vehicle configurations. Test vehicles may include high performance and general aviation aircraft, re-entry spacecraft, submarines and other fluidic vehicles. The measured data from forced oscillation testing is used in damping characteristic studies and in simulation databases for control algorithm development and performance analyses. The newly developed FOS hardware provides new flexibility for conducting dynamic derivative studies. The design is based on a tracking principle where a desired motion profile is achieved via a fast closed-loop positional controller. The motion profile for the tracking system is numerically generated and thus not limited to sinusoidal motion. This approach permits non-traditional profiles such as constant velocity and Schroeder sweeps. Also, the new system permits changes in profile parameters including nominal offset angle, waveform, and associated parameters such as amplitude and frequency. Most importantly, the changes may be made remotely without halting the FOS and the tunnel. System requirements, system analysis, and the resulting design are addressed for a new FOS in the 12-Foot Low-Speed Wind Tunnel (LSWT). The overall system including mechanical, electrical, and control subsystems is described. The design is complete, and the FOS has been built and installed in the 12-Foot LSWT. System integration and testing have verified design intent and safe operation. Currently it is being validated for wind-tunnel operations and aerodynamic testing. The system is a potential major enhancement to forced oscillation studies. The productivity gain from the motion profile automation will shorten the testing cycles needed for control surface and aircraft control algorithm development. The new motion capabilities also will serve as a test bed for researchers to study and to improve and/or alter future forced oscillation testing techniques.
Document ID
20060028241
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Trieu, B. C.
(NASA Langley Research Center Hampton, VA, United States)
Tyler, T. R.
(NASA Langley Research Center Hampton, VA, United States)
Stewart, B. K.
(NASA Langley Research Center Hampton, VA, United States)
Chamock, J. K.
(NASA Langley Research Center Hampton, VA, United States)
Fisher, D. W.
(NASA Langley Research Center Hampton, VA, United States)
Heim, E. H.
(NASA Langley Research Center Hampton, VA, United States)
Brandon, J.
(NASA Langley Research Center Hampton, VA, United States)
Grafton, S. B.
(Vigyan Research Associates, Inc. Hampton, VA, United States)
Date Acquired
August 23, 2013
Publication Date
May 1, 2006
Publication Information
Publication: 38th Aerospace Mechanisms Symposium
Subject Category
Mechanical Engineering
Distribution Limits
Public
Copyright
Public Use Permitted.
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