Test Method for Traction Turning Performance Verification of Fixed Wing UAV

This paper analyzes the factors influencing the traction turning performance of medium and large fixed-wing UAVs. By utilizing the basic theories of mechanics and mathematics, it establishes an experimental configuration analysis method based on the critical state of overturning. Additionally, it develops auxiliary identification, data processing, and analysis methods for ground traction turning tests of fixed-wing UAVs. These advancements address the issues of complex configuration and susceptibility to operator influence during ground towing turning of large and medium fixed-wing UAVs. The research provides an effective methodological support for the performance verification tests of traction turning for large and medium fixed-wing UAVs.