文档介绍：南京航空航天大学硕士学位论文
摘要
飞/推综合优化控制技术采用优化计算机实时接收飞机和发动机的信息,利
用内嵌的优化模块,对发动机控制指令进行修正,使飞机和发动机的整体性能达
到最优。
本文首先在保持原有 TMS320VC33 DSP + CPLD 硬件框架不变的基础上,通过
加入 TL16C554 串口扩展芯片和更新 CPLD 逻辑扩展芯片,对最初的基于
TMS320VC33 DSP 的优化计算机硬件系统进行了扩展改进,并完成了实物在回路
仿真验证。
为了进一步提高飞/推综合控制优化计算机的运算速度和集成度,提出了基
于 TMS320C6713 和 TMS320F2812 双 DSP 平台的优化计算机硬件架构,并对其具体
电路进行了详细设计,研制出了基于双 DSP 平台的优化计算机原理样机。然后研
究了基于双 DSP 平台的优化计算机的软件开发流程,完成了 SCI 异步串口通讯和
HPI 主从机接口通讯的测试程序设计和硬件测试。测试结果表明采用双 DSP 架构
可以显著提高优化计算机的运算速度和运行稳定性,也验证了该优化计算机设计
方案是可行的。
关键词:航空发动机,飞/推综合控制,优化计算机,双 DSP,定点 DSP,浮点
DSP,SCI,HPI 接口
I
基于双 DSP 平台的飞/推综合控制优化计算机设计
ABSTRACT
The overall performance of airplane and aero-engine can be optimized by
applying the technology of Integrated Flight / Propulsion Control (IFPC) in a
puter, where the modified control instructions is calculated for the
engine controller based on the informations from the airplane and the aero-engine.
Through appending the munications element (ACE)
TL16C554 and plex Programmable Logic Device (CPLD), the first
edition puter which processor is TMS320VC33 DSP is improved
greatly. And the result of Hardware-in-Loop simulation indicates that serial
communication can satisfy the puter requirements.
In order to increase operation speed and integrate degree of optimization
computer, the two-core hardware frame in which TMS320C6713 and TMS320F2812
are adopted is presented in this paper. At the same time Detailed circuit design and
particular principle machine design are given too. Then researched the software
design process based on puter of double DSP and maded a series of
experiments about SCI munication and munication. The result of
these experiments indicates that the two-core hardware frame could enhance operation
speed and the stability of puter remarkably.
Key Words: aero-engine, integrated flight/propulsion control (IFPC), optimization
computer, double DSP,fixed-point DSP, floating-point DSP,SCI, host port interf