Design and analysis of a two-loop autopilot;

To design the three-loop autopilot properly,the characteristics and operation principle have been analyzed.

A three-loop autopilot of the pitch/yaw mix channel is designed using optimal control;meanwhile the singular value of the open-loop system is tested in frequency domain,to have the robustness of the system insured,and the obtained three-loop autopilot has the characteristic of simple structure,so it is more practical.

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.