关键词: 飞行控制系统, 非线性控制, 非线性鲁棒控制, 鲁棒补偿, 参数不确定性

Abstract:

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.

Key words: flight control systems, nonlinear control, nonlinear robust control, robust compensation, parameter uncertain