FIELD: aircraft engineering.
SUBSTANCE: proposed system comprises onboard system of radiotelemetric measurements including the following components: data acquisition system, transducers of flight parameters, aircraft systems operation, encoding unit and radiotelemetric system transmitter, and measuring complex installed on the surface that comprises: radiotelemetric system receiving stations, system of outer-trajectory measurements, universal time system, communication lines, flight experiment control station comprising: data input unit, computation complex including local computation network of light info real-time computer-based processing system, computation complex integrated into local display and control computation circuit including, in its turn, automated workstations of test leader and control team specialists as well as means for radio communication with tested aircraft crew and operative-command communication with aforesaid measuring complex.
EFFECT: higher efficiency and safety of test flight.
1 dwg
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Authors
Dates
2013-03-10—Published
2012-03-30—Filed