摘要
本文利用非线性系统的最优控制理论,直接采用非线性飞机动力学模型设计了一组次优非线性增稳控制规律,并且讨论了这组控制规律对大机动飞机动态特性的影响.
This paper presents the design of suboptimal nonlinear stability augment control law for nonlinear aircraft dynamic model by optimal control theory of nonlinear system, how this control law effects the dynamic behavior of aircraft during vapid maneuvering flight is discussed.
出处
《飞行力学》
CSCD
北大核心
1990年第4期86-92,共7页
Flight Dynamics