. Airborne radar. Airplanes; Guided missiles. 650 DISPLAY SYSTEM DESIGN PROBLEMS logical factors indicated that there might be an interaction between the radar noise level and the scale factor used on the scope. An experiment was therefore designed in which the amplitude of the radar noise, the scope scale factor and the frequency of data inputs to the system were the variables. The results of this study are summarized in Fig. 12-33. The. 0 2 4 6 8 10 12 NOISE-RMS mils (a). Please note that these images are extracted from scanned page images that may have been digitally enhanced for readabilit
. Airborne radar. Airplanes; Guided missiles. 650 DISPLAY SYSTEM DESIGN PROBLEMS logical factors indicated that there might be an interaction between the radar noise level and the scale factor used on the scope. An experiment was therefore designed in which the amplitude of the radar noise, the scope scale factor and the frequency of data inputs to the system were the variables. The results of this study are summarized in Fig. 12-33. The. 0 2 4 6 8 10 12 NOISE-RMS mils (a). Please note that these images are extracted from scanned page images that may have been digitally enhanced for readability - coloration and appearance of these illustrations may not perfectly resemble the original Povejsil, Donald J. Princeton, N. J. , Van Nostrand
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Keywords: ., bookcentury1900, bookcollectionbiodiversit, booksubjectairplanes
