Systém automatického řízení letu pro lehké sportovní letouny

autopilot, primary flight display with touch controlled user interface,
multifunction display, navigation, control, micro controller, electromechanical
actuator, automatic propulsion control, autotrim

The present invention relates to an automatic flight control system for light
sports airplanes comprising a primary flight display with touch user interface
connected to an aircraft control system with manual and automatic means of flight
control and with a network of board sensors of system, flight and navigation data
and further comprising a multifunctional display. Said primary flight display
with touch user interface comprises a first microcomputer in the form of an on
chip system, which is connected to a visual display unit with plat touch sensor,
forming a display and control surface of the primary flight display, wherein said
on chip system is further connected to a real-time microcontroller and the
primary flight display is further connected by means of connectors to an aircraft
data network, which incorporates a system of electromechanical actuators for
automatic control of the aircraft control surfaces, an automatic control of
propulsion in the aircraft automatic flight control mode and for automatic
balancing control.