ae105c cdr, june 3, 2009 p. 1 ae105c term project cdr team report from experimental team jason...
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Ae105c CDR, June 3, 2009 p. 1
Ae105c Term ProjectCDR
Team report from
Experimental TeamJason CerundoloVivek ViswanathanPelayo Bohorquez
Ae105c CDR, June 3, 2009 p. 2
Level 2 Requirements
Level 2 – Experimental Team Specific Provide experimental data, including geometry, material property, static, and dynamic data, used to verify a structural finite element model (FEM).
Ae105c CDR, June 3, 2009 p. 3
Interfaces
•Will be put into master matrix in appropriate spots.
Ae105c CDR, June 3, 2009 p. 4
Assumptions
All tests must be non-destructive. Filters on hardware electronics do not affect data in region of interest. – Verified by manufacturers' datasheets. The filter
cut-off frequency is much higher than region of interest.
Motion of boundary condition is negligible. – Valid assumption because motion of canister during
testing was below the noise floor. The boom's response is in the linear stress-strain region. – This is driven by the System ID and Structural teams'
models and influences experiments that are run and the processing of the data.
Ae105c CDR, June 3, 2009 p. 5
Synopsis up to PDR
Geometry and material properties measurements were completed and published.
Static test were completed and in process of being published and processed.
Brainstormed ideas for dynamic testing
Ae105c CDR, June 3, 2009 p. 6
Disposition of RFAs
RFA / Concern Recommendation Action Taken
#2: Address resolution of measurements
Look at specs for lasers and requirement for precision
Measurements from lasers are accurate to about 1 μm. Precision required by other teams was not specified and assumed to be sufficient.
#6: Interfaces not aligned
Teams meet to scrub interfaces
Met with teams, specifically System ID and Structural, and clarified experiments to be completed.
#7: Level 1,2 requirements not set
Specify level 1 and 2 requirements
Met as a class and determined level 1 and 2 requirements for each team.
Ae105c CDR, June 3, 2009 p. 7
Progress Since PDR
Static test parameters have been published Dynamic testing completed
Random vibration Sine sweep Tap Test Ambient Test Torsion Test
Experimental descriptions, parameters, and data posted online and linked to from the wiki.
Ae105c CDR, June 3, 2009 p. 88
Technical Status
All testing and publishing is completed. Experimental results have met or exceeded the requirements of the other teams.
Ae105c CDR, June 3, 2009 p. 99
General Experimental Setup
Canister firmly mounted on pipe structure with racketed tie-down straps.
Laser displacement sensors measure vertical and horizontal displacement.
Shaker is attached to center of endplate. – The shaker moves a given displacement
for a given input voltage using feedback.
– A load cell measures the force applied by the shaker.
– Low load cell measurements imply modes. Signals from sensors are processed by input boxes and captured on a PC running LabView under Windows Vista.
Tests run multiple times to ensure repeatability.
Ae105c CDR, June 3, 2009 p. 1010
General Experimental Setup
Ae105c CDR, June 3, 2009 p. 1111
Static Force-Displacement Test
• Known masses were hung by the center of the end plate.
• Deflection of the boom at multiple points was measured.
• Force-displacement curve could be fit to stiffness.
Ae105c CDR, June 3, 2009 p. 1212
Random Vibration Test
• Shaker is given random noise from function generator.
• Data was not used in analysis – The function
generator excited up through 50 MHz.
– Region of interest was 1 – 100 Hz, only a small amount of energy was exciting those frequencies.
– This resulted in an insufficient signal-to-noise ratio.
Ae105c CDR, June 3, 2009 p. 1313
Sine Sweep Test
• Shaker is sine wave input swept through a frequency range (5 – 100 Hz).
• Time scale was logarithmic and around 4 octaves/minute.
• FFT of displacement over FFT of load cell data show modes of vibration.
• Mode found near 15 Hz.
Ae105c CDR, June 3, 2009 p. 1414
Tap Test
• Structure is excited by a manual tap with a hammer.
• The ring down response is measured. – Allows easy
calculation of damping.
– Ideally shows fundamental mode.
Ae105c CDR, June 3, 2009 p. 1515
Ambient Test
• Structure is left undisturbed and response measured.
• This test gives a good indication of the noises environment in the lab.
• Can identify unexpected modes and identify regions of noise.
Ae105c CDR, June 3, 2009 p. 1616
Torsion Test
• Shaker was mounted off-axis and connected to one of the longerons not on the vertical axis of symmetry
• Lasers were positioned off-axis.– Difference in
position is the torsion.
• Mode found near 50 Hz.
Ae105c CDR, June 3, 2009 p. 1717
Open Issues and Concerns
Random noise test has insufficient signal-to-noise ratio.
– FFT of ambient matched random noise. – Compensated by sine sweep testing. – Recommend a narrow band-limited function
generator to supply random noise in the future. • Current set up is limited to 50 MHz. • Region of interest is only up to 1 kHz.
Test Conducted with imperfect boundary condition.
– Recommend detailed study of canister mount be conducted in the future.
– Recommend a more isolating mount be used. Tap Test
– Force hammer would provide more data and allow for another check of results.
– For now, only good for damping
Ae105c CDR, June 3, 2009 p. 18
Summary
Testing specified by level 2 requirements is complete. Geometry and material property
Provided at sufficient fidelity to Structural Team Static
Force-displacement– Used to correlate with Structural Team's model.
Dynamic Random vibration
– Used to identify regions of interest and rough estimates of mode frequencies.
Sine sweep– Chosen over random noise due to higher signal-to-noise ratio. – Used by System ID Team to correlate modes with computerized
models. Ambient noise
– Used by System ID Team to remove lab environment noise from other tests.
– Improved fidelity of data from other dynamic tests. Tap response
– Used by System ID Team to deduce damping response. Torsion
– Used by System ID Team to identify torsional modes and correlate with computerized models.
Ae105c CDR, June 3, 2009 p. 19
Back-up Material
Ae105c CDR, June 3, 2009 p. 20
Equipment Used
Equipment Manufacturer Model Notes
Laser Head KeyenceLK-G157 & LK-G87
Displacement sensor
Laser Controller
Keyence LK-GD500
Signal Generator
Agilent 33250AGenerate input signal for force shaker
Power Amplifier Labworks Inc. PA-138
Force Sensor PCB 208C01 a.k.a. “Load Cell”
Vibration Motor Labworks Inc. ET-132 a.k.a. “Shaker”
Signal Conditioner
PCB 480E09
Analog to Digital Converter
National Instruments
NI USB-6210
Data Collection Program
National Instruments
LabView 8.6Running on Windows Vista
Post Processing MATLab 2009bRunning on various operating systems