The stability analysis of assembly process was implemented from the two respects of the stability of components assembled and the stable location and pose of moving subassemblies.

To design the flight attitude stability control loop of gun-launched unmanned aerial vehicle(UAV) with longitudinal and lateral directional 2D linear model established in terms of the static stability condition during the cruise,the improved proportional feedback control method is employed to achieve the require of the settling time and steady-state precision.

So the attitude stability of robot has been made the further requst.

The autokinetic attitude stabilization of a synchronous satellite;

Nonlinear control of attitude stabilization of an underactuated spacecraft

To study the attitude stabilization control effect on short-range antitank rockets using pulse jets.

The posture stabilization problem of nonholonomic wheeled mobile robots is studied using this method,and the simulation results verify the validity of this method.