Disclosed is a flight control system for a VTOL aircraft comprising a first and a second manual control apparatus for inputting control commands by an operator, a flight control computer, which is connected to the first and second manual control apparatuses and configured to output flight control instructions based on pivot positions of the first and second stick members with respect to the first to fourth control axes, wherein the flight control computer is adapted to derive and output flight control instructions, while at least partially eliminating cross-coupling between the individual directions of motion for longitudinal motion control based on the pivot position of the first stick member with respect to the first control axis.
FLIGHT CONTROL SYSTEM AND METHOD FOR A VTOL AIRCRAFT
2024-10-03
Patent
Electronic Resource
English
Automatic flight control for VTOL aircraft
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