The invention relates to the technical field of aircraft testing, in particular to a comprehensive
avionics test bench for an electric vertical take-off and landing multi-rotor aircraft. Comprising a base, a support, a
test platform, an arm test module and an upper computer. The base is connected with the bottom of the bracket; the top of the bracket is connected with the
test platform; the arm test module is connected with the
test platform; the base is used for fixing the
test bench; the support is used for supporting the testing platform. The test platform and the arm test module are used for testing
avionics of the aircraft; the upper computer is used for controlling the test mode of the
test bench. According to the invention,
modular design is adopted, disassembly and
assembly can be realized, expansion can be realized, a group of motor assemblies can be tested, multiple groups of motor assemblies can be tested, a whole
machine can be tested, power can be supplied by using a battery, an external power supply can be used,
remote control and wire control can be realized, and various
test requirements can be realized.