电光与控制, 2010, 17 (4): 53, 网络出版: 2010-06-22  

飞行参数实时采集系统的设计与实现

Design and Implementation of a Real-Time Flight Parameter Acquisition System
作者单位
北京航空航天大学 仪器科学与光电工程学院,北京 100191
摘要
为了准确获取实时的飞行参数,提出了一种以FPGA为核心的多路数据采集系统设计。描述了系统硬件设计,通过VerilogHDL语言设计有限状态机完成流水采样以及FPGA与DSP数据通信,并用Modelsim对各设计模块进行仿真。实验证明这种设计方法简化了系统的硬件电路复杂性,使整个采集系统具有灵活高效的特点。
Abstract
In order to collect real-time flight parameters accurately, the design of a multi-channel data acquisition system was proposed using FPGA as the core. The system hardware design was described. Pipeline sampling and data communication between FPGA and DSP were both realized by Finite State Machine described in VerilogHDL, and the design modules were simulated by Modelsim. Experiment proved that this design simplifies the complexity of the hardware circuit and makes the data acquisition system possess a flexible and efficient characteristic.

刘鑫, 李成贵, 孟召宗. 飞行参数实时采集系统的设计与实现[J]. 电光与控制, 2010, 17(4): 53. LIU Xin, LI Chenggui, MENG Zhaozong. Design and Implementation of a Real-Time Flight Parameter Acquisition System[J]. Electronics Optics & Control, 2010, 17(4): 53.

关于本站 Cookie 的使用提示

中国光学期刊网使用基于 cookie 的技术来更好地为您提供各项服务,点击此处了解我们的隐私策略。 如您需继续使用本网站,请您授权我们使用本地 cookie 来保存部分信息。
全站搜索
您最值得信赖的光电行业旗舰网络服务平台!