Robust terminal sliding mode control for ASV re-entry mode;

Aerodynamics prediction and configuration optimizati on for reentry vehicle with double-ellipse cross-section;

Fluctuating response analysis of reentry vehicles;

Unscented Kalman Filtering for Reentry Vehicle Tracking;

Study on modeling of re-entry vehicle signatures;

An autopilot design scheme is presented with feedback linearization technique against the fast time varying, strong coupling and high nonlinear system of the high speed reentry aerocraft dynamics.

Also the autopilot of reentry aerocraft was designed with this nethod.

High-speed reentry aerocraft is usually with terminal guidance system.

Maneuverability Analysis of Reentry Vehicles Based on Moving Centroid Control Mode

In this paper,basing on three-axis\'s stable dynamic equations of moving centroid reentry vehicles,the dynamic inversion controller was designed under three-axis\'s stable control mode.

Moving centroid control for reentry vehicles is used to realize the maneuvering control by changing the center of mass of reentry vehicles and aerodynamic trim torque,so as to adjust the flying attitude and angle of attack.

Design of a fuzzy adaptive trajectory linearization controller for an aerospace vehicle;

Design of a predictive control law for re-entry aerospace vehicles;

Flight control for an aerospace vehicle s reentry attitude based on thrust of reaction jets;