摘要
设计了一种基于古典控制理论的新型自适应飞行控制系统 ,对其设计方案进行了仿真论证 ,并对这种自适应控制飞行系统与古典飞行控制系统进行了比较 。
A new adaptive flight control systems is designed based on classic control,and its design scheme is simulated and demonstrated.The superiority of the adaptive control system is manifested in comparison with the classic flight control system.
出处
《战术导弹技术》
2002年第5期46-49,共4页
Tactical Missile Technology
