FIELD: instrument engineering.
SUBSTANCE: system can be used for controlling flying vehicles. Motion parameter detector is introduced into the system additionally. Input/output of the detector is connected with data exchange line. Computational system has closing error forming unit, speed of wind estimating unit, wind speed predicting unit, speed vector back calculating unit, speed vector re-projecting unit and angle of attack and slip angle calculating unit.
EFFECT: widened operational capabilities.
1 dwg
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Authors
Dates
2005-10-27—Published
2004-03-23—Filed