控制增稳系统改善飞机横航向模态特性的能力  

CAS IMPROVE A CAPABILTY OF AIRCRAFT FOR LATERAL-DIRECTIONAL MODE RESPONSE

作　　者：刘振钦 

机构地区：[1]西安飞机设计研究中心

出　　处：《飞行力学》1989年第3期60-65,共6页Flight Dynamics

摘　　要：本文对有无控制增稳系统飞机的横航向模态特性进行了比较计算.通过计算对系统进行了数学分析,从而得到了一组较佳的系统参数,提高了系统改善飞机横航向模态特性的能力.In this Paper, the contents of a CAS (Control Augmentation System) and without CAS of aircraft lateral-directional mode response were computed and compared. Through computing, the system was analysed of methematical, a group better parameter of system were acquired, the system improve a capability of aircraft for lateral-directional mode response was increase.

关 键 词：增稳系统 飞机 模态特性 

分 类 号：V212.12[航空宇航科学与技术—航空宇航推进理论与工程]