ZHANG Tao, WANG Xiao-hua, ZHA Shi-hong, CHEN San-feng, ZHANG Wei-zhong, MEI Tao. On Aircraft Mass Simulation Method under Space Micro Gravity Environment[J]. ROBOT, 2008, 30(6): 528-530,535.
Citation: ZHANG Tao, WANG Xiao-hua, ZHA Shi-hong, CHEN San-feng, ZHANG Wei-zhong, MEI Tao. On Aircraft Mass Simulation Method under Space Micro Gravity Environment[J]. ROBOT, 2008, 30(6): 528-530,535.

On Aircraft Mass Simulation Method under Space Micro Gravity Environment

  • Based on the 6-DOF micro gravity and micro friction space environment simulation device,a mass compensa- tion method based on floatation technology is proposed which combines pneumatic technology with floatation technology. The presented method effectively solves the mass variation problem of the simulated spacecraft in different directions,and provides a theoretical basis for simulation on the characteristics of aircraft mass and rotary inertia.
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