Using auto-disturbances-rejection-controller(ADRC),a new scheme is proposed to design an aircraft super-maneuverable flight controller in a big flight envelope.

This paper describes a neural network based direct adaptive control approach to the problem of reconfigurable flight control of a super-maneuvering aircraft.

Then the super-maneuver airplane is controlled according to the established model to get the simulation result.

Research on robust and adaptive nonlinear control system of supermaneuverable fight;

An approach to neural network-based robust and adaptive dynamic surface control is proposed for supermaneuverable flight with violent changes of aerodynamics parameters.

A neural network based method for compensating dynamic inversion error is introduced in this paper and is applied in the control of a supermaneuvering aircraft.

An adaptive dynamic inversion controller design method based on neural network(NN) is proposed for super maneuverable fighter aircrafts.

Research on Super-maneuverable Flight Control of Fighter and Multi-fighter Cooperative Multi-target Attack Technology;

Then based on the singular perturbation theory,the super-maneuverable flight control system is divided into two loops: fast loop.

On Designing of Driving and Control System for Traveling Wave Ultrasonic Motor;

In this paper a summarized account is first made on the principle and characteristics of ultrasonic motors, the recent achievements in the field of control technology for ultrasonic motors are introduced, then comparisons are performed among these achievements and the advantages and the disadvantages of the existing control technology are analyzed.

The article first briefly reviews the developing history of ultrasonic motor, then it puts emphasis on the introduction of its current domestic & overseas research situation and suggests its engineering appliction field.