Aeronautics and Space Institute (IAE), DCTA, Brazil
By Vid Selič, NVH engineer, Dewesoft
At the Aeronautics and Space Institute (IAE), DCTA, structural dynamic tests, like sine processing, SRS and modal analysis are performed as a part of the standard procedure on different components of rocket launch systems. In this case, the nose cone of a rocket was tested on a shaker using sine processing.
Dewesoft X software improved the time efficiency and the quality of data acquired by supporting the real-time calculation through a designated sine processing user interface.
The Departamento de Ciência e Tecnologia Aeroespacial (DCTA), the Brazilian Department of Science and Aerospace Technology is located in São José dos Campos – the largest Aerospacial Complex in all Latin America.
DCTA functions as the Brazilian national military research center for aviation and space flight and subordinated to the Brazilian Air Force (FAB) and coordinates all technical and scientific activities related to the aerospace sector involving interests of the Ministry of Defense.
Testing took place at Instituto de Aeronaútica e Espaço (IAE), the Aeronautics and Space Institute. This institute develops and executes projects in the aeronautical, airspace and defense sectors, and is co-responsible for the execution of the Brazilian Space Mission.
The nose cone tested in this particular structural test plays an important role in R&D activities conducted for TEXUS missions - a sounding or research rocket program, serving the microgravity programs of the European Space Agency (ESA) and Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), the German Aerospace Center.
The IAE part of the TEXUS missions focuses primarily on the development of the launch systems intended for and facilitating the exploration of the properties and behavior of materials, chemicals, and biological substances under weightless conditions (micro gravitation). Each launch provides around six minutes of microgravity.
In this case, IAE needed to measure the resonance frequencies of their rocket nose cone in order to avoid operation in these frequencies, which could compromise the structural integrity and potentially cause mission failure.
They needed a reliable data acquisition system capable of tracking and computing the defined range of responses and transfer functions in real-time.
Sine processing and Sine Reduction Test Case
Sine processing is a tool to perform structural tests on large structures. Such testing approach is widely used for design validation and qualification in the aerospace industry, and typically, hundreds of input channels are required.
By definition, there is no room for error, all structures utilized during a mission must be carefully tested beforehand to ensure proper operation and uncompromised structural integrity.
Different modes resulting from excitation in resonance frequencies
The evaluation of such large structures is done by exciting them with a sweep of single frequencies on a shaker. Sine Sweep Vibration Testing traverses or sweeps from low to high frequency or vice versa. It is used to identify resonances inside the range of the sweep by comparing response vibrations of the product to the vibrations on the shaker table.
As desired output, sine processing returns the following:
- structural resonance frequencies,
- total harmonic distortion (THD) of response and also
- transfer functions between excitation and response points.
In order to evaluate the structure under test in the frequency domain, it is important to accurately extract these parameters from the sinusoidal signal.
Sine processing uses a Constant Output Level Adaptor (COLA) signal to calculate instantaneous frequency and then extracts amplitude and phase from the accelerometers at that frequency. The COLA signal output synchronizes the shaker control system with the DAQ system.
At IAE/DCTA the Dewesoft X data acquisition software – with the sine processing plugin - and Dewesoft SIRIUS data acquisition system was used for the data acquisition.
The sine processing test runs by synchronizing the Dewesoft data acquisition system with the vibration shaker controller (3rd party). The Dewesoft sine processing tool performs one of the two methods of frequency detection:
Acquired signals from accelerometers placed on the rocket nose cone are measured together with sweep frequency which is detected from the COLA signal. They are then computed in real-time to provide detailed insight into the structure’s response to excitation.
Test and Measurement Setup
To ensure results relevant for the customer, it was important to perform a sine sweep test from 25-1000Hz, which is the typical frequency range of vibration which a rocket nose cone will undergo during transport, launch, and flight.
For the data acquisition, we were using a system with two SIRIUSi-HD-16xACC slices. The DAQ system offered 32 IEPE accelerometer inputs in total. The same DAQ system also enables IAE/DCTA to perform other measurement tasks and also offers an easy way to extend the input channel count. Additional inputs like IEPE, voltage, temperature, strain gage and others can be added easily to form a high channel count system when needed.
To showcase Dewesoft sine processing solution true power, we were running also 1/3rd octave analysis and true FFT with 4096 lines resolution (the selectable line resolution allows up to 64.000 lines) simultaneously with sine processing on all 31 channels. The only exception being was the input channel used for the COLA signal from the vibration shaker controller.
The sine processing itself runs inside Dewesoft X DAQ software, including the ability to connect and measure other useful parameters, such as environmental conditions of the test or include high-speed video to observe how DUT is moving during the test.
8 triaxial accelerometers were attached to the nose cone structure (outer dimensions fi 874mm x 1830mm) in configuration to obtain the best possible desired results.
For the test, we were using five Brüel & Kjaer triaxial accelerometers and three PCB accelerometers. Seven accelerometers were placed along with the shape of the structure, and serving as a reference one PCB triaxial accelerometer was placed on the adapter attaching the nose cone to the shaker table.
One analog input on our two SIRIUSi-HD-16xACC was used to connect the COLA voltage signal for frequency detection of the sweep transmitted from the shaker controller to the shaker and exciting the structure.
The SIRIUS DAQ systems also include two very important technologies that bring measurements and data acquisition to the next level:
- Galvanic isolation
DualCoreADC - High Dynamic DAQ
SIRIUS DAQ amplifiers use two 24-bit AD converters for signal conditioning. The SIRIUS is achieving an astonishing 160 dB dynamic range in time and frequency domain with a 200 kHz sampling rate per channel.
The DAQ system also offers high channel-to-channel and channel-to-ground isolation which prevents unwanted noise, offers the best signal quality and prevents damage to the systems from excessive voltage and avoids ground loops.
The device under test was excited in the direction of the shaker table movement and our coordinate system was placed correspondingly so that the y-axis was aligned with the axis of excitation.
The test stand: The positioning of the accelerometers: 7 on the rocket nose cone under test and 1 one the adapter plate attached to the shaker bed
IAE/DCTA was already using a designated system for the tests and was handling all the transfer function calculations in post-processing. The Dewesoft sine processing plugin is able to handle the calculation of transfer functions, phase, RMS, Peak and a lot of other parameters in real-time.
Results calculated in real-time are vital for IAE as DUTs such as rocket launch systems and/or payloads are costly. IAE engineers get immediate insight into the measured parameters of the structure, allowing them to directly monitor if resonance frequencies and corresponding amplitudes are within expected/projected values
Additional calculations, not selected to be performed in real-time, can be performed in post-analysis using the time domain data that was stored during the measurement.
IAE Test engineer, Domingos Strafacci concluded:
The system is really easy to use and setup. It will save us a lot of time when performing this kind of crucial structural testing.
The measurement that took place, in this case, was only using a single of many nodes that would otherwise be building a larger system. It must be noted, however, that regardless of the number of channels the operational properties of the system will remain unchanged.
As DCTA research and development activities consist of many different projects, they are able to benefit greatly from the advantages of structural testing and the flexibility of Dewesoft system, that can be used to perform many tasks such as road data vibration acquisition and GPS tracking of the route, modal analysis on the wing of a plane or SRS measurement during rocket stages separation test.
The IAE dynamic tests leader, Dr. Edilson Camargo said:
As this system is very flexible it will enable us to tackle a variety of our day to day measurement tasks, not just sine processing. Through this, we will be able to optimize our cost expenditure.