nav emailalert searchbtn searchbox tablepage yinyongbenwen piczone journalimg journalInfo journalinfonormal searchdiv searchzone qikanlogo popupnotification paper paperNew
2021, 03, v.44 163-171
晶振对飞行器时频同步系统的影响
基金项目(Foundation): 中国科学院青年创新促进会资助项目(1188000WHB)
邮箱(Email):
DOI: 10.13875/j.issn.1674-0637.2021-03-0163-09
摘要:

飞行器时频同步系统采用双向伪距测量,伪距信息通过测量信号到达时间获得。由于晶振在飞行平台上处于振动和动态状态,与地面静态场景受到的影响不同,因此对晶体振荡器的选择和应用十分重要。本文介绍了晶振老化率、晶振频偏的影响,构建了由各类误差源引起的跟踪环路误差模型。仿真结果表明,振动引起的晶振相位噪声和阿伦偏差晶振相位噪声随环路带宽增大而减小,随环路阶数增大而增大;选用高稳定度,g敏感度小的晶振可降低环路跟踪误差;将阿伦偏差作为晶振选择的指标具有较大的实用意义。

Abstract:

The flight vehicle time-frequency synchronization system uses bi-directional pseudo-range measurement, and the pseudo-range information is obtained by measuring the signal arrival time. The crystal oscillator is in vibration and dynamic state on the flight platform, which is affected differently from the static scene on the ground, so it is very important for the selection and application of crystal oscillator. In this study, the effects of crystal oscillator aging rate and crystal oscillator frequency bias are introduced, and the tracking loop error model caused by various error sources is constructed. The simulation results show that the phase noise of crystal oscillator caused by vibration and Allan's deviation decreases with the increase of loop bandwidth, and it increases with the increase of loop order; the selection of crystal oscillator with high stability and small sensitivity can reduce the loop tracking error; the Allan's deviation as the index of crystal oscillator selection has a greater practical significance.

参考文献

[1]冯雪阳.基于GPS秒脉冲的恒温晶振驯服和自适应保持技术研究与实现[D].成都:电子科技大学, 2014.

[2]宋东风.高动态环境中INS辅助GNSS接收机测速误差分析[D].长沙:国防科学技术大学, 2013.

[3]王嘉琛,樊多盛,肖波,等.基于晶振的远程时间同步参考源性能分析[J].时间频率学报, 2020, 43(4):270-278.

[4]王振凯.基于晶体谐振器等效参数的老化补偿研究与系统实现[D].西安:西安电子科技大学, 2018.

[5]王宏兴.高阶温度补偿晶体振荡器设计[D].西安:西安电子科技大学, 2018.

[6]江金光,唐亚男,李姗姗.基于单片机的晶振温度补偿系统设计[J].压电与声光, 2016, 38(3):492-496.

[7]叶羽铭.一种压控温补晶体振荡器(VCTCXO)的设计和实现[D].成都:电子科技大学, 2020.

[8]谢亦龙.星载晶体振荡器抗振设计[D].成都:电子科技大学, 2019.

[9]孙成城.高稳定度晶体振荡器的低老化率及补偿问题研究[D].西安:西安电子科技大学, 2013.

[10]赵岩,李智奇,周渭,等.晶体振荡器的频率稳定度和老化特性研究[J].时间频率学报, 2018, 41(3):267-275.

[11] WANG X, JI X, FENG S, et al. A high-sensitivity GPS receiver carrier-tracking loop design for high-dynamic applications[J].GPS Solutions, 2015, 19(2):225-236.

[12]谢钢. GPS原理与接收机设计[M].北京:电子工业出版社, 2009.

[13] PARKINSON B W, JR J J S, AXELRAD P, et al. Global Positioning System:Theory and Applications[M]. Volume I. Washington:American Insitute of Aeronautics and Astronautics, Inc, 1996.

[14] TREES H L V. Detection, Estimation, and Modulation Theory, Part II:Nonlinear Modulation Theory[M]. USA:Wiley, 2002.

[15]韩舒文,原海军,左启耀,等.晶振误差特性及其对弹载卫星导航接收机的影响分析[J].导航定位与授时, 2017, 4(3):66-71.

[16]卡普兰. GPS原理与应用[M].寇艳红,译. 2版.北京:电子工业出版社, 2007.

基本信息:

DOI:10.13875/j.issn.1674-0637.2021-03-0163-09

中图分类号:V249

引用信息:

[1]李辉,吴华兵,赵当丽.晶振对飞行器时频同步系统的影响[J].时间频率学报,2021,44(03):163-171.DOI:10.13875/j.issn.1674-0637.2021-03-0163-09.

基金信息:

中国科学院青年创新促进会资助项目(1188000WHB)

发布时间:

2021-07-15

出版时间:

2021-07-15

检 索 高级检索

引用

GB/T 7714-2015 格式引文
MLA格式引文
APA格式引文