In this paper,a simple method for solving analytical solutions of attitude autopilots closed-loop characteristic equation is proposed.

Error compensation with multiple sensors in a MEMS autopilot;

Research on the Intelligent Fault Diagnosis Method of a Certain Missile Autopilot;

Development of autopilot technology of small UAV;

Design of breakdown diagnose fuzzy-expert system for shore-to-ship missile automatic pilot;

An intelligent automatic pilot for the flight control of missiles by regulating is studied.

A new data sampling and processing software developed by Visual C_(++) based on Windows operating system is introduced for automatic pilot auto-testing system which is made by oneself.

Research of Using Aerodynamic/Reaction-jet Controller for Designing Missile Autopilot;

In this paper, the H∞ robust performance design method for the systems with mixed uncertainty is briefly introduced, and the problem of missile autopilot design is deeply studied.

Inherent characteristic of lateral acceleration autopilot is studied.