The Application of Modified Output Error Method and Its Verification.
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Amodified output error method developed by the authors are presented, and an example of its application on the YF16 aircraft is shown. The method is originally developed for the purpose of analyzing an air accident. As the method has been proven to be quite effective, we hoped to apply it to the other aircraft's flight data for estimating the aerodynamic cnaracteristics and the input control histories. As there were no data available at hand, we first produced the flight data by simulations, then applied the method whether we can reproduce the aerodynamic characteristics and input control histories. The employed aircraft is YF16 about which the fairly detailed data are published. The result shows that the method is very effective to this purpose.