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车载便携式气压高度计的设计 被引量:3

The Design of Vehicle-Borne Baro-Altimeter
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摘要 针对航空电子设备车载试验缺乏独立高度测量数据,无法充分模拟机载环境的缺陷,本文利用芬兰VTI公司SCP1000-D01传感器芯片完成了基于USB接口的气压高度计设计。通过该气压高度计进行低空数据采集分析,文中得出气压高度计在较短测量时间内具有良好的稳定性,高度差值更精确的特点。这与高空飞行数据的气压高度测量数据分析结论相一致,表明该便携式气压高度计能够弥补现有车载试验缺乏独立高度测量的缺陷,并具备低成本、方便灵活的优点。 The paper presents design of a kind of USB - based baro - altimeter which employs SCP1000 - 1901 sensor chi Pof VTI Corp. , Finland. The baro - altimeter is used to solve a realistic problem that vehicle - borne experiment of aviation electronic instru- ments is lack of independent altitude measurement data and airborne environment cannot be simulated completely. Based on data col- lection in low- altitude air, a conclusion is drawn that this baro- altimeter has good stability in short- time measurement, with more accurate altitude difference. This is consistent with the conclusion drawn from analysis of flight baro - altimeter measurement data in high - altitude air. It indicates that this baro - alimeter is able to provide independent altitude measurement data in vehicle - borne experiment, with low cost and enough flexibility.
作者 李锐 姚怡
出处 《微计算机应用》 2010年第4期43-47,共5页 Microcomputer Applications
基金 科技部973项目(No.2010CB731800) 自然基金课题(No.60979013)资助
关键词 气压高度 高度差值 SCP1000-D01传感器 baro - altitude, altitude difference, SCP1000 - D01 sensor
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参考文献5

  • 1RTCA DO- 229D, Minimum Operational Performance Standards for Global Positioning System/Wide Area Augmentation System Airborne Equipment[ S]. D. C. Washington: RTCA,2001.
  • 2陈家斌,袁信.气压高度表辅助下GPS接收机自备完善性监测可用性研究[J].航空学报,1996,17(5):561-565. 被引量:12
  • 3Shau - Shiun J. , Demoz G. E. , Todd W.. Worst - Case Analysis of a 3 - FrequencyReceiver to Land a General AviationAirplane [ A ]. Proceedings of the 15th International Technical Meeting of the Satellite Division of The Institute of Navigation [ C ]. Fairfax, VA : The Institute of Navigation, 2002. 2576 - 2586.
  • 4宫晓琳,房建成,盛蔚.一种GPS与高精度气压高度表在线互标定方法[J].电子与信息学报,2009,31(4):818-821. 被引量:7
  • 5李锐.机载无源北斗组合导航设备定位关键技术研究[D].北京:北京航空航天大学,2005.

二级参考文献13

  • 1耿延睿,崔中兴,张洪钺,房建成.衰减因子自适应滤波及在组合导航中的应用[J].北京航空航天大学学报,2004,30(5):434-437. 被引量:22
  • 2范小军,刘锋.一种新的机动目标跟踪的多模型算法[J].电子与信息学报,2007,29(3):532-535. 被引量:32
  • 3Wang T. Barometric altimeter short-term accuracy analysis[J]. IEEE A&E Systems Magazine, 2005, 20(12): 24-26.
  • 4Gray R A and Maybeck P S. An integrated GPS/INS/BARO and radar altimeter system for aircraft precision approach landings[C]. IEEE Proceedings of the Aerospace and Electronics Conference, Dayton, 1995, 1: 161-168.
  • 5Mahapatra P R and Mehrotra K. Mixed coordinate tracking of generalized maneuvering targets using acceleration and jerk models[J]. IEEE Trans. on Aerospace and Electronic Systems, 2000, 36(3): 992-1000.
  • 6Zhou H and Kumar K S P. A current statistical model and adaptive algorithm for estimating maneuvering targets[J]. Journal of Guidance, Control and Dynamics, 1984, 7(5): 596-602.
  • 7以光衢.航空机载电子系统与设备[M].北京:北京航空航天大学出版社,1997:44-46.
  • 8Xia Q J, Rao M, and Ying Y Q, et al.. Adaptive fading kalman filter with an application[J]. Automatica, 1994, 30(12): 1333-1338.
  • 9Levent O and Aliev F A. Comment on adaptive fading Kalman filter with an application[J]. Aautomatica, 1998, 34(12): 1663-1664.
  • 10Lee Y C,J Institute of Navigation,1993年,40卷,2期,179页

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