FIELD: aviation.
SUBSTANCE: based on the telemetric information on the operation of the onboard inertial navigation system (INS) and on-board satellite navigation equipment (SNE), as well as data on the coordinates of the point of the aircraft fall (AC) and the moment of the AC collision with the ground surface, the corrections are a posteriori determined that coordinate the measured and calculated data, on the basis of which the motion (translational and rotational) variables are recovered in the atmospheric phase of the AC. At the same time, a highly accurate determination of the actual (experimental) variables of the (translational and rotational) motion of the atmospheric phase is provided.
EFFECT: enhanced functional capacity.
2 dwg
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