摘要
通过分析飞控系统各环节对飞机动态特性的影响及第三代战斗机控制律的特点,为战斗机综合设计仿真系统建立了飞控系统模型。该模型是能够反映飞控系统功能的简化模型。通过对飞控系统各项功能与特点的检验,对飞控系统简化模型进行了验证。验证结果表明,所建立的简化飞控系统模型能够满足战斗机综合设计仿真系统的需要。
By analyzing the effects of every part of a flight control system （FCS） on the dynamics of the aircraft, and the characteristics of the 3^rd generation fighter＇s FCS, the FCS of the fighter integrated design simulation system is modeled. Such model is a simplified model,which can indicate the characteristics and functions of the FCS. The simplified model is validated by verifying the main characteristics and functions of the FCS. The results indicate that the simplified model can satisfy the requirements of the fighter integrated design simulation system.
出处
《飞行力学》
CSCD
北大核心
2006年第4期22-25,29,共5页
Flight Dynamics
关键词
综合设计
仿真系统
飞控系统
简化模型
integrated design
simulation system
flight control system
simplified model
