A GNSS Antenna Layout Evaluation Method for Hypersonic Vehicle

被引：0
|
作者：
Wang, Ruihong [1 ]
Wu, Yongliang [1 ]
Gong, Youmin [1 ]
机构：
[1] Aviat Ind Corp China, AVIC Chengdu Aircraft Design & Res Inst, Chengdu, Peoples R China
来源：
2018 EIGHTH INTERNATIONAL CONFERENCE ON INSTRUMENTATION AND MEASUREMENT, COMPUTER, COMMUNICATION AND CONTROL (IMCCC 2018) | 2018年
关键词：
Hypersonic Vehicle; Satellite Navigation; Antenna Layout Evaluation; STK/Matlab;
D O I：
10.1109/IMCCC.2018.00265
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
Due to hypersonic vehicle's high velocity, large attitude maneuver and wide envelope, unreasonable antenna layout will lead to bad performance of satellite navigation, such as the reduction of received GNSS satellite numbers or even non-positioning. In this paper, a GNSS antenna layout evaluation method for hypersonic vehicle is proposed to handle this problem. A hypersonic vehicle mission simulation and GNSS antenna layout evaluation environment based on STK/Matlab is established to validate the method, including the aircraft's typical trajectory and attitude data, navigation satellite constellation, and two different antenna layout models. The advantages and disadvantages of the two antenna layouts are analyzed. Based on the proposed method, the proper antenna layout which meets the flight safety and mission requirements is found out by calculating the receiving satellite numbers and PDOP of the GNSS receiver.
引用
收藏
页码：1278 / 1282
页数：5
相关论文
共 50 条
  • [41] Forebody compressibility research of hypersonic vehicle
    Liu Jia
    Yao Wen-xiu
    Lei Mai-fang
    Wang Fa-min
    Applied Mathematics and Mechanics, 2004, 25 (1) : 93 - 101
  • [42] The Adaptive Fuzzy control of Hypersonic Vehicle
    Guan Ping
    Xue Li
    Liu Xiao-he
    Wang Sai
    PROCEEDINGS OF THE 2012 24TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC), 2012, : 2722 - 2727
  • [43] Fuzzy Control Design for Hypersonic Vehicle
    Li, Guo
    Lv, Xiaoliang
    PROCEEDINGS OF THE 2016 4TH INTERNATIONAL CONFERENCE ON MACHINERY, MATERIALS AND COMPUTING TECHNOLOGY, 2016, 60 : 1361 - 1366
  • [44] An Experimental Study of a Hypersonic Waverider Vehicle
    WU Ding-yi
    International Journal of Plant Engineering and Management, 2008, 13 (04) : 200 - 204
  • [45] Forebody compressibility research of hypersonic vehicle
    Liu, J
    Yao, WX
    Lei, MF
    Wang, FM
    APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION, 2004, 25 (01) : 93 - 101
  • [46] A nonlinear control approach for a hypersonic vehicle
    Tao, Chao
    Wan, Jing
    Ai, Jianliang
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2017, 89 (02) : 320 - 329
  • [47] Combined thermal phenomena of hypersonic vehicle
    Gui YeWei
    SCIENTIA SINICA-PHYSICA MECHANICA & ASTRONOMICA, 2019, 49 (11)
  • [48] Method for improving the precision of hypersonic vehicle inertial navigation system based on neural network
    Xu Y.
    Xian Y.
    Li B.
    Ren L.
    Li S.
    Guo W.
    Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics, 2022, 44 (04): : 1301 - 1309
  • [49] Identification Method of SINS Error Parameters Utilizing Artificial Neural Network for Hypersonic Vehicle
    Guo, Weilin
    Xian, Yong
    Zhang, Daqiao
    Wang, Zhaoqiang
    IEEE ACCESS, 2019, 7 : 165820 - 165841
  • [50] Prescribed Performance-based Lateral Channel Control Method of Underactuated Hypersonic Vehicle
    Wang, Xiaofang
    Xu, Jiaqi
    Binggong Xuebao/Acta Armamentarii, 2024, 45 (08): : 2749 - 2760
12345