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空间飞行器
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  spacecraft
This collection can be used to test spacecraft production materials, in order to determine their resistance to biodegradation.
      
Studying Stability of the Flexible Spacecraft with a Discrete Control System
      
Stability of the spacecraft was considered with regard for its elastic structural oscillations arising under discrete control.
      
Consideration was given to the possibility of estimating jointly the motion coordinates and parameters of the elastic spacecraft using algorithms based on the discrete Kalman filtering and the theory of testing statistical hypotheses.
      
Design of the Suboptimal Profiled Relay Control of Orientation of the Spacecraft Having Elastic Structural Elements with Regard
      
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Presented is an analysis of the dynamics of a mechano electronic spring damper system of differential type applied in the docking mechanism of space craft. An algorithm for dynamical analysis of this coupled 6 degree of freedom system with both serial and parallel connections was presented. Dynamic equations of the system were derived by using Lagrangian technics. The constraint equations were given. Columb frictions which can be found between many parts of the system were dealt with in a special way....

Presented is an analysis of the dynamics of a mechano electronic spring damper system of differential type applied in the docking mechanism of space craft. An algorithm for dynamical analysis of this coupled 6 degree of freedom system with both serial and parallel connections was presented. Dynamic equations of the system were derived by using Lagrangian technics. The constraint equations were given. Columb frictions which can be found between many parts of the system were dealt with in a special way. An example was carried out. Dynamical analysis, the analysis of the stiffness and damping characteristics and the function analysis for validation can be performed with the method presented.

研究了用于空间飞行器对接机构的差动式机电缓冲阻尼系统的动力学。提出了一种关于此类6自由度的串、并联复合系统的动力学分析方法。应用Lagrange分析技术推导出了系统动力学方程,给出了相应的系统约束方程,并对系统中多部位的库仑摩擦阻尼进行了处理和实例计算分析。结论表明该方法可进行差动式机电缓冲阻尼系统的动力学分析、系统刚度和阻尼特性分析以及系统功能校核分析。

 
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