文档介绍：南京航空航天大学
硕士学位论文
无人飞行器发动机控制系统设计与实现
姓名:于鉴
申请学位级别:硕士
专业:飞行器设计
指导教师:徐锦法
20080301
南京航空航天大学硕士学位论文
摘要
航空发动机作为无人飞行器的动力来源其动静态性能将直接影响无人飞
行器的飞行品质发动机控制是飞行控制系统的前提与基础同时也是实现无
人飞行器自主飞行的关键良好的发动机控制系统离不开相关硬件设备和控制
软件的支持本文就是针对无人飞行器发动机控制开展软硬件系统及其控制律
设计实现的研究
首先根据发动机控制的需求设计了发动机控制系统的组成结构和功能
其次分析系统对硬件的要求选择了机载计算机传感器数据通信和地面
站等硬件设备并构建发动机控制硬件系统在分析比较并确定具体的软件
开发环境基础上开发完成了实时性好可靠性高的机载发动机控制器程序
以及功能完善操作简便并具有较好移植性的地面站操控和监视软件接着
引入自适应PID控制思想设计了发动机自适应PID控制器使得发动机在不同
工况时控制参数能够进行自适应调节达到改善控制效果的目的最后采
用发动机试车的方法对发动机控制系统的性能和功能进行检验并使用半物理
仿真的方法验证自适应PID控制器的控制效果所得结果满足无人飞行器飞行控
制要求

关键词无人飞行器发动机控制软硬件平台自适应 PID 发动机试车
半物理仿真
i
无人飞行器发动机控制系统设计与实现
Abstract
Aero-engine is the power source of Unmanned Air Vehicle (UAV), its dynamic
and static characteristics directly affect the performances of UAV. Engine control is
the foundation of UAV flight control system, and the key factor to realize autonomous
flight. An excellent Engine Control System (ECS) doesn’t exist without the supports
of corresponding hardware and control algorithm. This paper focuses on the design
and implementation of software and hardware and the design of ECS control law.
Firstly, the constituent parts, the architecture and the functions of ECS were
designed according to the requirements of engine control. Secondly, the requirement
analyses about hardware were made, the devices such as flight puter,
sensors, data-link units and ground control station were selected, and then the
hardware architecture of ECS was achieved. Through analyses parisons of
different software development environments, the appropriate one was chosen. By
using it, the airborne programs of engine controller with real-time performance and
reliability were developed; the control and monitoring software running on ground
station with perfect functions, easy operations and convenient transplantation were
then developed. Thirdly, the adaptive PID control concepts were introduced to design
an engine controller