"Multi-rotor UAV flight control system semi-physical simulation test method" provides a semi-physical simulation test method for functional performance and safety of flight control samples. Functional performance physical-in-the-loop simulation tests include: hardware-in-the-loop takeoff and landing, hardware-in-the-loop control mode switching, hardware-in-the-loop flight control testing, one-key return and autonomous landing; safety semi-physical simulation tests include: gyroscope fault injection, acceleration Meter fault injection, magnetometer fault injection, motor fault injection, sensor communication interruption, motor communication interruption and remote control communication interruption fault.
T/SZUAVIA 003(1)-2023 history
2023T/SZUAVIA 003(1)-2023 Semi-physical simulation test method for the flight control system of multi-rotor unmaned aircraft