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 landi...
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| creator | HU YAHANG ZANG ZIYI MA JINGYA LI HAIYUE WANG GUOXING CHENG ZE CHEN YANPING |
| description | 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 |
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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. 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| subjects | AIRCRAFT AVIATION COSMONAUTICS DETECTING MASSES OR OBJECTS GEOPHYSICS GRAVITATIONAL MEASUREMENTS MEASURING PERFORMING OPERATIONS PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR |
| title | Mars rover solar wing low-gravity simulation test device and test method |
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