In addition to the guidance provided in Part One, paragraphs 5.14 and 5.17, and Part One, Annex A, Tasks 405 and 406, the following information is provided to assist in the evaluation of the test results. Analyze in detail any failure of a test item to meet the requirements of the system specification, and consider related information such as:
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a. Proper collection of information from the control accelerometer configuration, including representative durations of time trace information at all test levels based on expressions for estimate statistical error criteria. All time trace measurement information must be time-correlated to ensure proper estimation.
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b. Proper collection of information from the monitor accelerometer configuration (if any), including representative durations of time trace information at all test levels according to the same principles as used for control measurements.
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c. Record the vendor MET software test tolerance information.
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d. If necessary, apply one or more of the techniques described in Annexes C and D for detailed comparison of the frequency domain information. In particular, use the collected time trace information to compute the agreed-upon test metrics.
527.2-5 DATA REQUIRED
As discussed in NATO AECTP Leaflet 24103, field data must be acquired based upon the anticipated mission scenario of the unit under test (UUT). As detailed in paragraph 4.4.1.1 and reference number 1, transducer placement and orientation are critical and must be thoroughly documented.
5.1 Physics of Failure
Analyses of vibration related failures must relate the failure mechanism to the dynamics of the failed item and to the dynamic environment. It is insufficient to determine that something broke due to high cycle fatigue or wear. It is necessary to relate the failure to the dynamic response of the materiel to the dynamic environment. The scope and detail of analysis should be coordinated with and approved by the appropriate test authority. It is recommended to include in the failure analysis a determination of resonant mode shapes, frequencies, damping values, and dynamic strain distributions, in addition to the usual material properties, crack initiation locations, etc.
527.2-5.1 Reference SDM Development
As stated in paragraph 4.5, a SDM in terms of the desired rigid body modes to be tested should be computed for each test configuration identified in the mission scenario.
5.1.1 SDM Ensemble CSD Characteristics
Based on the characteristics of the CSD terms of the ensemble of SDMs, the VSD process will yield a vibration specification consistent with one of the three cases that follow:
- a. Case 1. Coherence Terms Approaching Zero (Independent Motion DOFs) – This is the easiest situation to deal with in that each motion DOF ASD may be addressed individually via the same techniques employed in 1-DOF VSD as discussed in reference number 3. When programming the vibration control system, it is recommended that coherence be set to a low non-zero level (i.e. ) over the test bandwidth of interest. For such a small coherence, the phase parameter is essentially a random variable and establishing a phase specification is not required.
A special situation that may lead an analyst to develop a MDOF vibration specification with independent motion DOFs, would be a composite specification that encompasses multiple vehicles (i.e. a composite wheeled vehicle specifications comparable to those in MIL-STD-810H, Method 514.8). As each vehicle will tend to have its own CSD characteristics, it is not possible to define CSD terms such that a single coherence and phase relationship addresses each vehicle. Enveloping techniques that work well in addressing magnitude based ASD terms are simply not applicable in addressing phase relationships between mechanical DOFs.
- b. Case 2.Non-Zero Coherence across a Portion of the Test Bandwidth – When developing a MDOF vibration specification based on a single platform, one would expect the CSD terms measured across the range of scenarios addressed in the mission scenario to be similar in nature. The dynamic characteristics of the structure and often the proximity of the measurement transducers will greatly influence the CSD characteristics. There are often situations in which coherence between motion DOFs are high and phase is well defined, but only over a portion of the test spectrum. This is a common observation on many wheeled vehicles where coherence is high at lower frequencies (i.e. frequencies below 50 Hertz (Hz) and near zero at higher frequencies. In such scenarios, one would only establish coherence and phase specifications for the portion of the spectrum with high coherence. The remainder of the spectrum would be treated as in Case 1. Also, in establishing CSD reference criteria, the analyst must ensure the resulting criteria is physically realizable (refer to paragraph 4.5.3 for additional detail).
- c. Case 3. Non-Zero Coherence across the Full Test Bandwidth – This scenario is comparable to Case 2 with coherence being defined across the entire test bandwidth. It is anticipated that this would be the least likely scenario in a MDOF VSD effort. However, it is also the configuration that will be the most difficult to deal with from both a VSD development aspect and from an implementation perspective. In addition to the issue of ensuring the resulting SDM reference is physically realizable, the classic problem of mechanical impedance mismatch between field and laboratory are often major concerns in implementing a fully defined SDM reference criterion for a laboratory test. Specifically, if the mechanical impedance between field and laboratory are not very well matched (and they usually are not), there may be portions of the spectrum in which coherence may be significantly different than specified and simply not controllable. While this situation is also possible in Case 2, it is almost certain to be an issue in a scenario such as Case 3, in which the entire test bandwidth has a CSD reference criteria. This topic of uncontrollable coherence associated with mechanical impedance mismatches is a control issue for all three Cases and is discussed further in the minimum drive consideration of paragraph 4.5.6.
- d. Regardless of which of the three cases the SDM is characterized by, it is highly likely that there will be mechanical impedance differences between the field and laboratory conditions. In some cases these impedance differences may result in excessive drive signals. Although the various control system vendors
MIL-STD-810H METHOD
5.2 Qualification Tests
When a test is intended to show formal compliance with contract requirements, recommend the following definitions:
- a. Failure definition. “Materiel is deemed to have failed if it suffers permanent deformation or fracture; if any fixed part or assembly loosens; if any moving or movable part of an assembly becomes free or sluggish in operation; if any movable part or control shifts in setting, position, or adjustment, and if test item performance does not meet specification requirements while exposed to functional levels and following endurance tests.” Ensure this statement is accompanied by references to appropriate specifications, drawings, and inspection methods.
- b. Test completion. A vibration qualification test is complete when all elements of the test item have successfully passed a complete test.
527.2-5.2 Test Tolerance Recommendations
Setting tolerances for a MIMO test is challenging given the large amount of information encompassed by the reference autospectra and cross spectra involved. Additionally, the overall energy is not necessarily distributed evenly about each mechanical DOF and dominant DOFs often tend to dominate the control. The objective here is to establish a reasonable starting point in establishing test tolerances. Experience with specific test configurations may be employed to refine the basic guidance defined below. As usual, any test specific test tolerances should be clearly documented within the test plan.
- a. Autospectra for and for .
(1)The portion of the spectrum that actually reaches the maximum tolerance limits is anticipated in narrow bandwidths. The tolerance on the overall Grms level of each controlled DOF shall be within ±15% of the corresponding reference.
- b. Cross spectra: Define tolerances in terms of Phase and Coherence. Note that there will be a statistical variation of coherence and phase estimates as a function of the statistical DOFs used to estimate the control SDM and also as a function of the coherence between inputs. Take caution in that the expected statistical variation imposes a lower limit on how tight the respective tolerance can be. The coherence and phase guidance given below should be used in the absence of tolerances determined from field environments and necessary margin needed to account for laboratory and in-field service mechanical impedance mismatches. Note that there may be scenarios in which coherence and phase tolerances need not be defined for the entire test bandwidth.19
- (1) Coherence: For ordinary coherence in the range , set the tolerance to be (avoid establishing a coherence reference or tolerance of 1.0).
- (2) Phase: If , any phase is acceptable. If and the frequency is within the band where is a frequency where the reference rate of phase change is more than and is the line spacing of the reference spectra, the default tolerance on phase will be . Otherwise, if outside of a frequency band referenced with such high rates phase change, the default tolerance on phase will be .
- c. Limiting: See paragraph 4.5.4.
5.3 Other Tests
For tests other than qualification tests, prepare success and/or failure criteria and test completion criteria that reflect the purpose of the tests.
527.2-5.3 Laboratory Data
In the case the reference SDM is directly employed as the reference in a MET test (i.e. input/output (I/O) Transformation Control as discussed in reference number 9), and rigid body presumptions are sound, the control accelerometers are not required to be placed in the exact same location in the laboratory as they were used in the original acquisition phase. The critical parameter is that all control locations employed in the laboratory test are referenced to the same “origin” as selected in the original VSD development. However, it is often desirable, based on making position specific comparisons between field and laboratory data, to match the laboratory control locations to the original measurement points.