FIELD: testing equipment. SUBSTANCE: proposed system includes aircraft simulator, radio altimeter simulator, control point simulator and control signal generation unit. System is also provided with angular rate sensor simulator, angle meter simulator, linear acceleration meter simulator, actuating mechanism simulator, wind gust simulator, underlying surface simulator and observation object coordinate meter simulator, as well as observation object parameter setter, fly-by monitoring unit and test results processing unit including selector switch, memory switch, implementation holding unit, accuracy estimation computer and collision probability computer and indicator. All these components are respectively interconnected. EFFECT: increased scope of tests of equipment; enhanced reliability of ground tests at lesser labor consumption. 11 dwg
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Authors
Dates
2001-02-27—Published
2000-06-09—Filed