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I__. - International Military Testing Association

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Valuable time of experts is saved by having the model compute intermediate<br />

data elements.<br />

Paramters. The parameters identified in table 3 were selected to make<br />

the model flexible, i.e., capable of simulating conditions where the<br />

relative importance of the variables listed can be changed at will by the<br />

analyst. By using a computer terminal, the analyst may input alternative A,<br />

8, C, D, E, or F to establish the relative importance of the variables in<br />

determining expected trials-to-mastery. Relative importance of these<br />

variables is expected to vary from one aircraft community to another.<br />

,<br />

Table 3<br />

Parameters for Weighting Trials-to-Mastery<br />

Parameter Relative Importance<br />

Addftive Method<br />

A Instructors Students Tasks<br />

8 -Students Instructors Tasks<br />

Tasks Instructors Students<br />

s Instructors Tasks Students<br />

Students Tasks Instructors<br />

s Tasks Students Instructors<br />

The mean trials-to-mastery for the experimental and control groups,<br />

obtained by the interactive method, are used as a basis for the values used<br />

in the the additive method. Here the same expert is asked to estimate<br />

trials-to-mastery for each of the conditions one at a time. The questions<br />

are phrased as deviations around the mean trials-to-mastery (table 4).<br />

Training experts estimate six conditions in each group, a total of 12<br />

conditions. The remaining 42 values (representing the difference between 12<br />

and 54) are estimated by the computer model according to the rules of<br />

additive conjoint measurement (Lute & Tukey, 1964).<br />

Reljabilitv Check<br />

Since each training expert is asked for inputs to the model by two<br />

different methods, a check on methodological variance is possible by<br />

correlating the values obtained by the interactive and additive methods (N =<br />

54). This correlation fs computed across methods for experimental and<br />

control groups.<br />

SUMMtYOFMOOEL FLOU<br />

Input, output, and<br />

figure 1 and figure 2.<br />

interactive aspects of the mode1 are summarized in<br />

194<br />

4

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