FIELD: tool-making industry, possible use in onboard systems for automatic control of unmanned aircrafts under conditions of their broad usage regarding flight speed and height.
SUBSTANCE: in accordance to the invention, the control system contains flight height sensors, flight speed sensors, angle, angular speed and current mass sensors, banking angle setting unit and two support signal setting units, comparison block, executive device, two adders, two division blocks, block for forming reverse value of signal, three scaling blocks, digital multiplication block, digital-analog converter and digital-analog multiplication block.
EFFECT: expanded functional capabilities of system due to increased stability and precision of control processes.
1 dwg
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