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METHOD OF MEASUREMENT OF EARTH gravity anomalies in laboratory WORKS AND DEVICE FOR ITS IMPLEMENTATION

机译：实验室工作中地球重力异常的测量方法及其实现方法

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1. A method for measuring the earth's gravitational field anomalies (GPP) and other planets for laboratory work based on the use of a spacecraft (KA), framed flywheel orientation and stabilization system, located on a circular orbit, measuring its coordinates and the angles determining the oscillation stabilization KA characterized in that the spacecraft at a certain analysis interval T, the monitoring portion comprising GPP through flywheel orientation and stabilization system is introduced in a self-oscillating mode with the following parameters: ! amplitude KA φ0 = 45 °, corresponding to self-oscillation detection maximum impact of the GEA, including its anomalies in the dynamics of the spacecraft! phase oscillations v0 = 0, defined by the condition of the initial combination of its own satellites and forced vibrations,! self-oscillation frequency ωp! ! wherein Jx, Jy, Jz - the moments of inertia about respective axes KA; ! - gravitational parameter - the value of the gravitational parameter; ! μ = 398 602 km3 / s2 - Earth's gravitational constant; ! RKA = R3 + h - the radius of the spacecraft orbit! where rg - Earth radius (spherical shape rg = 6371 km); ! H - height of the circular orbit satellites; ! K1, K2 - the coefficients of the law of formation of control moment orientation and stabilization system at a channel pitch! and, based on a comparison of the differences stabilization oscillation amplitudes: ! where θi * - the actual values ​​of the AC oscillation stabilization in pitch channel on analysis interval T i-th time instants; ! θ0 ij - modeling values ​​obtained by solving the equation of motion of the model with different values ​​of j-mi gravitational parameter ω2 0j; ! i = 1, 2, ... N, the current time point in the analysis interval T in which the cf.
机译：1.一种用于测量地球重力场异常（GPP）和其他行星以进行实验室工作的方法，该方法基于使用位于圆形轨道上的航天器（KA），带框架的飞轮定向和稳定系统，测量其坐标和角度确定振荡稳定KA，其特征在于，航天器以一定分析间隔T，通过飞轮定向和稳定系统由GPP组成的监视部分以自振荡模式被引入，其具有以下参数：振幅KAφ0= 45°，对应于GEA的自激振动检测的最大影响，包括其在航天器动力学中的异常！相位振荡v0 = 0，由其自身卫星和强迫振动的初始组合的条件定义！自激频率ωp！ ！其中Jx，Jy，Jz-绕各个轴KA的惯性矩; ！ -重力参数-重力参数的值; ！ μ= 398602 km3 / s2-地球重力常数; ！ RKA = R3 + h-航天器轨道的半径！其中rg-地球半径（球形rg = 6371 km）; ！ H-圆形轨道卫星的高度; ！ K1，K2-通道间距下控制力矩方向和稳定系统的形成定律！并且，基于差的比较，稳定振荡幅度为：其中θi*-分析间隔T i次时刻上音调通道中AC振荡稳定的实际值; ！ θ0ij-通过求解j-mi引力参数ω20j不同值的模型的运动方程获得的建模值; ！ i = 1、2，... N，是分析间隔T中的当前时间点，其中cf。

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