Dual spacecraft observations of energetic particles in the vicinity of the magnetopause,bow shock,and the interplanetary medium

This article presents some of the new and important particle features that have been detected in the energy range 1 keV to 290 keV by the ISEE-1 and -2 spacecraft near the magnetopause, bow shock, and the interplanetary space. Only examples of data from the first few orbits, when the spacecraft were on the front side, are shown.Paper presented at 13th ESLAB Symposium, Innsbruck, Austria (June 5, 1978).     

Modeling the motion of an uncompensated gyrostabilized platform in the Rodrigues-Hamilton parameters

We construct a model of triaxial gyrostabilizer platform motion at the force stabilization regime. The Rodrigues-Hamilton parameters have been chosen as kinematic parameters describing the changes in the gyrostabilized platform state vector. The advantages of using the model constructed in the initial attitude control systems of inertial navigation systems as compared with the existing ones are shown.     

Theory of an annular corrugated damper in the vibrator precession motion

The theory for calculating elastodamping characteristics of multilayer corrugated dampers being used in the rotor supports of aircraft gas turbine engines (GTEs), turbo-pump assemblies of rocket engines as well as in different articles of machine building industry is presented.     

System sensitivity to parametric variations in the problem of lateral motion flight vehicle control

The results of investigation of dynamic system sensitivity to parametric variations in the channel of flight vehicle lateral motion are presented using the notion of infinitesimal transformation. The exact relationships establishing a link between the structure of parameter deviation and that of system phase coordinate deviation are obtained.     

非均匀栅距对轴流压气机流动影响的数值研究

本文进行了非均匀栅距叶片排的轴流式压气机流场数值研究,进口导叶采用了不同的非均匀栅距结构,探讨了不同工作状态下对压气机性能及动叶非定常气动力的影响。数值研究中采用LU-SGS隐式解法与双时间方法相结合,求解圆柱面二维流动的雷诺平均非定常N-S方程。数值研究的结果表明,进口导叶非均匀栅距结构对压气机气动性能影响不大,但对动叶表面受到的非定常气动力有一定影响。采用不同的非均匀栅距进口导流叶片排结构型式,动叶表面的非定常气动力的分布是不同的。不同工作状态下的计算结果显示,即使采用相同的非均匀栅距结构,非定常气动力的分布特性也是不相同的。