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基于DSP的嵌入式导航计算机分布式系统设计 被引量:10
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作者 黄丽斌 周百令 单茂华 《中国惯性技术学报》 EI CSCD 2003年第4期16-19,共4页
为满足MIMU/GPS组合导航系统的小型化、低功耗、低成本等条件,以及越来越高的精度要求,以TI公司TMS320VC5402型DSP器件为核心,设计了一种嵌入式导航计算机分布式系统。此设计可提高系统的精度,更好地满足系统实时性要求。
关键词 DSP MIMU/GPS组合导航系统 嵌入式导航计算机分布式系统 设计 数字信号处理器
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基于Profibus现场总线的智能大厦保安管理系统
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作者 高伟 吴俊林 《西安工程科技学院学报》 2002年第2期148-151,共4页
介绍了 Profibus现场总线技术在智能大厦的保安管理系统中应用 ,分析了该系统的结构配置及功能特点 .该系统运用结果表明 ,Profibus为实现工厂自动化和设备智能化提供了可行的解决方案 。
关键词 智能大厦 保安管理系统 现场总线 PROFIBUS 计算机分布式系统
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NOVEL AIRCRAFT ELECTRICAL POWER DISTRIBUTION SYSTEM BASED ON DISTRIBUTED COMPUTER 被引量:3
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作者 杨善水 付大丰 严仰光 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2001年第2期224-228,共5页
As a matured technique used in many fields,the distributed computer system is still a new management method for the aeronautical electrical power distribution system in our country. In this paper, a novel aircraft ele... As a matured technique used in many fields,the distributed computer system is still a new management method for the aeronautical electrical power distribution system in our country. In this paper, a novel aircraft electrical power distribution system based on the distributed computer system is proposed. The principles, features and structure of the aircraft electrical power distribution system and the distributed computer system named electrical load management system (ELMS) are studied. The ELMS composed of four electrical load management centers (ELMCs) and two power source processors (PSPs) operates in the 1553B buses. Principles of the ELMCs and the PSPs are introduced. With the application of the distributed computer system, the aircraft electrical power distribution system is simple, adaptable and flexible. 展开更多
关键词 aircraft electrical power supply system aircraft electrical power distribution system distributed computer system 1553B buses electrical load management system
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PARAMETER IDENTIFICATION OF LUGRE FRICTION MODEL FOR FLIGHT SIMULATION SERVO SYSTEM BASED ON ANT COLONY ALGORITHM 被引量:4
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作者 段海滨 王道波 +1 位作者 朱家强 黄向华 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2004年第3期179-183,共5页
In light of the high nonlinearity of LuGre friction model, a novel method based on ant colony algorithm(ACA) for identifying the friction parameters of flight simulation servo system is proposed. ACA is a parallelized... In light of the high nonlinearity of LuGre friction model, a novel method based on ant colony algorithm(ACA) for identifying the friction parameters of flight simulation servo system is proposed. ACA is a parallelized bionic optimization algorithm inspired from the behavior of real ants, and a kind of positive feedback mechanism is adopted in ACA. On the basis of brief introduction of LuGre friction model, a method for identifying the static LuGre friction parameters and the dynamic LuGre friction parameters using ACA is derived. Finally, this new friction parameter identification scheme is applied to a electric-driven flight simulation servo system with high precision. Simulation and application results verify the feasibility and the effectiveness of the scheme. It provides a new way to identify the friction parameters of LuGre model. 展开更多
关键词 parameter identification LuGre friction mo-del flight simulation servo system
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