Mars rover solar wing low-gravity simulation test device and test method

The invention relates to a Mars rover solar wing low-gravity simulation test device and test method, which can simulate a landing attitude of a Mars rover and realize simulation of a Mars gravity environment in a solar wing unfolding process. The device comprises two functional units, namely a landing attitude simulation function unit and a Mars gravity simulation function unit. The landing attitude simulation function unit is a set of mechanical devices, simulates different attitudes of the Mars rover after landing by adopting a manual adjustment mode, and provides fixed support for the solarwing simulation wall at the same time. The Mars gravity simulation function unit is a set of gravity compensation devices, and a simulation effect of the Mars gravity acceleration in a ground environment is achieved by connecting a balloon and a solar wing mechanism and utilizing the buoyancy of the balloon. The device is small in occupied area, high in integration and convenient to operate, labor intensity can be reduce