综合飞行/推进关键自动模态设计与品质评价  

Integrated Flight/Propulsion Control Crucial Auto-modes Design and Performance Evaluation

作　　者：李亦楠[1] 张晶[1] 申功璋[1] 

机构地区：[1]北京航空航天大学控制一体化技术国家级重点实验室,北京100191

出　　处：《系统仿真学报》2010年第A01期103-106,共4页Journal of System Simulation

摘　　要：先进飞机的综合飞行/推进自动模态设计,是设计具有自动油门功能的自动驾驶系统,实现飞行速度的自动控制,使飞行员松开油门杆,实现真正意义的自动驾驶。以大型客机和运输机为背景,设计了综合飞行/推进关键自动模态,包括巡航模态、自动着陆模态、平飞加减速模态,实现姿态、速度和高度的保持与控制。同时分别给出了相应模态的飞行品质评价指标,利用该指标评价控制律设计结果。评价结果均满足相应模态飞行品质要求。The concept of integrated flight /propulsion control auto-modes design was to develop an autopilot/autothrottle control system which was able to accomplish automatic speed control. The employment of such system meant the implementation of real automatic flying and indeed reduced pilot’s workload. This paper presented integrated flight/ propulsion control auto-modes design of an advanced aircraft, including cruising mode, landing mode and height-holdspeed-control mode, as well as simulation and evaluation of this combined control system’s performance. And the results proved to be satisfied.

关 键 词：综合飞行/推进控制 自动模态 自动驾驶 飞行品质 

分 类 号：TP391.9[自动化与计算机技术—计算机应用技术]