Design of unmanned aircraft flight control system software based on uC/OS-Ⅱ operation system;

Integrating design of performance and reliability for flight control systems;

Survey of the active fault-tolerant control for flight control system;

In order to strengthen the anti-jamming of a certain UAV under electromagnetism circumstances and enhance the stability un- der permanent continuous work conditions,a certain innovative UAV flight control system(FCS)is designed which adopt C80515120(high -speed excellent performance SOC MCU),CPLD(Complex Programmable Logic Device),DUAL-PORT STATIC RAM.

This paper mainly concerns about the hardware design of Flight Control System(FCS) of a certain Unmanned Air Vehicle(UAV) , the improved design and software realization of a certain atmosphere data system(ADS).

Wavelength Division Multiplexing(WDM) technology,one of the critical technologies of fly-by-light (FBL) flight control system, was studied in terms of the characteristics of flight control systems.

The designing approach of nonlinear robust dynamic inversion for flight control systems is discussed, and a new control strategy with robust stability is presented, which will be needed to account for uncertain effects related with unknown parameters and external disturbance while in supermaneuver flight, and a stability result is got about this control strategy in case of parameters perturbation.

The eigenstructure assignment method is an efficient approach in designing multi-mode flight control systems ,which could determine the expected control law directly through integrating the system performance index with the flight quality requirements of aircraft.

Monte Carlo method is employed in longitudinal stability enhanced control law design and simulation process of a FBW flight control system in this paper.