gyroscope

The dynamical equations of a flexible spacecraft with VSCMGs(variable speed control moment gyroscopes) are established via the Lagrange equations in terms of quasi-coordinates and the momentum theorem.

利用拟坐标下的拉格朗日方程和动量矩定理,建立了带变速控制力矩陀螺群(VSCMGs,Variable Speed Control Moment Gyroscopes)的柔性航天器的能量/姿态一体化控制系统(IPACS,Integrated Power/Attitude Control System)的动力学模型,该模型适合于姿态控制律设计及VSCMGs操纵律设计。

Stabilization properties of airborne imaging platform based on position gyro and rate gyro;

航空光电成像平台角位置陀螺和角速率陀螺的稳定效果分析

Principle of the effect of gyro misalignment on the stabilization platforms accuracy;

陀螺安装误差影响视轴稳定平台精度的机理研究

Design and simulation of accelerometer based gyro-free inertial navigation system;

基于加速度计的无陀螺惯性导航系统设计与仿真

On-orbit calibration algorithm for gyros/star sensor;

陀螺/星敏感器在轨标定算法研究

On-orbit calibration algorithm with star sensors of gyros;

一种利用星敏感器对陀螺进行在轨标定的算法

a RBF neural network for gyro fault diagnosis of a placement of six one-freedom gyros is designed.

分析了径向基函数神经网络在陀螺故障诊断中的应用。

Electromagnetic induction pendulum and electromagnetic induction top;

电磁感应摆与电磁感应陀螺

Precession and nutation of top and gyrosscope is discussed by elementary method,equations of motion are solved using simplified models, and an elementary analysis is made.

用初等方法讨论了陀螺与陀螺仪的进动及章动,用简化模型求解了运动方程,并给出了它们的初等 分析。

A top is supported horizontally and the counterweight is connected by a spring,the direction of angular momentum of the top varies horizontally when the counterweight vibrates vertically.

给出了高速自转陀螺在连续周期性外力矩作用及力矩突变下的运动规律演示,实现了力矩可自动改变方向的角动量运动规律演示实验,还给出了在理论上角动量n次变化率不为零的一种实例演示。

Adaptive control design of MEMS gyroscope using stochastic averaging method;

基于随机平均法的MEMS陀螺自适应控制设计

Influence of the rotator’s spinning instability on the stability of Si micromachined gyroscope;

旋转体自旋角速度不稳定对陀螺稳定性的影响

Error analysis and integrated compensation of scale factor for MEMS gyroscope;

MEMS陀螺标度因数误差分析及分段插值补偿