FIELD: instrument engineering, applicable in automatic flight control systems for control of flight speed of remotely piloted flight vehicles, ground-effect machines, etc.
SUBSTANCE: the present flight speed and the linear acceleration relative to the flight vehicle longitudinal axis are measured, they are summed up, fluctuations caused by the wind gusts are compensated, a control signal proportional to the deviation of the present flight speed and the preset value is formed.
EFFECT: enhanced follow-up of the program-mission action.
2 dwg
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