Adaptive control design of MEMS gyroscope using stochastic averaging method;

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

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

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

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

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

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.

The domestic and foreign fault diagnosis methods for the gyroscopes and the latest development are analyzed and concluded.

On-orbit calibration algorithm for gyros/star sensor;

On-orbit calibration algorithm with star sensors of gyros;

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

Electromagnetic induction pendulum and electromagnetic induction top;

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.

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.