FIELD: equipment used at testing aircrafts. SUBSTANCE: system includes simulator of aircraft, radiosignal simulator and steering mechanisms whose outlets are connected with respective inlets of apparatus for simulating rolling motion of aircraft and to first inlet of apparatus for simulating pitching of aircraft. Angle detectors are mounted on platform of first dynamic stand, radar finder is arranged on platform of second stand. Radar finder, radio altimeter, angular velocity pickups, linear acceleration meters, control station simulator are connected with inlets of apparatus for generating control signals. System also includes simulator of angular motion of observed object. Angular velocity pickups are connected with first elasticity simulator, linear acceleration meters are connected with second elasticity simulator. Apparatus for generating control signals are connected through switching unit with steering mechanisms. EFFECT: enhanced accuracy of predicting results of nature testing of aircrafts. 6 dwg
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Authors
Dates
2001-02-20—Published
1999-06-07—Filed