Single-frequency L5 attitude determination from IRNSS/NavIC and GPS: a single- and dual-system analysis

被引:9
|
作者
Zaminpardaz, S. [1 ]
Teunissen, P. J. G. [1 ,2 ]
Nadarajah, N. [1 ]
机构
[1] Curtin Univ, Dept Spatial Sci, GNSS Res Ctr, Perth, WA, Australia
[2] Delft Univ Technol, Dept Geosci & Remote Sensing, Delft, Netherlands
基金
澳大利亚研究理事会;
关键词
IRNSS; NavIC; GPS Block IIF; Integer carrier-phase ambiguity resolution; Attitude determination; Multivariate-constrained integer least squares; MC-LAMBDA; INTEGER LEAST-SQUARES; LAMBDA METHOD;
D O I
10.1007/s00190-017-1033-y
中图分类号
P3 [地球物理学]; P59 [地球化学];
学科分类号
0708 ; 070902 ;
摘要
The Indian Regional Navigation Satellite System (IRNSS) has recently (May 2016) reached its full operational capability. In this contribution, we provide the very first L5 attitude determination analyses of the fully operational IRNSS as a standalone system and also in combination with the fully operational GPS Block IIF along with the corresponding ambiguity resolution results. Our analyses are carried out for both a linear array of two antennas and a planar array of three antennas at Curtin University, Perth, Australia. We study the noise characteristics (carrier-to-noise density, measurement precision, time correlation), the integer ambiguity resolution performance (LAMBDA, MC-LAMBDA) and the attitude determination performance (ambiguity float and ambiguity fixed). A prerequisite for precise and fast IRNSS attitude determination is the successful resolution of the double-differenced integer carrier-phase ambiguities. In this contribution, we will compare the performance of the unconstrained and the multivariate-constrained LAMBDA method. It is therefore also shown what improvements are achieved when the known body geometry of the antenna array is rigorously incorporated into the ambiguity objective function. As our ambiguity-fixed outcomes show consistency between empirical and formal results, we also formally assess the precise attitude determination performance for several locations within the IRNSS service area.
引用
收藏
页码:1415 / 1433
页数:19
相关论文
共 28 条
  • [1] Single-frequency L5 attitude determination from IRNSS/NavIC and GPS: a single- and dual-system analysis
    S. Zaminpardaz
    P. J. G. Teunissen
    N. Nadarajah
    Journal of Geodesy, 2017, 91 : 1415 - 1433
  • [2] IRNSS/NavIC and GPS: a single- and dual-system L5 analysis
    S. Zaminpardaz
    P. J. G. Teunissen
    N. Nadarajah
    Journal of Geodesy, 2017, 91 : 915 - 931
  • [3] IRNSS/NavIC and GPS: a single- and dual-system L5 analysis (sic)
    Zaminpardaz, S.
    Teunissen, P. J. G.
    Nadarajah, N.
    JOURNAL OF GEODESY, 2017, 91 (08) : 915 - 931
  • [4] IRNSS/NavIC L5 Attitude Determination
    Zaminpardaz, Safoora
    Teunissen, Peter J. G.
    Nadarajah, Nandakumaran
    SENSORS, 2017, 17 (02)
  • [5] Single-frequency L5 PPP-RTK with GPS, IRNSS, QZSS and Galileo
    Li, W.
    Nadarajah, N.
    Teunissen, P. J. G.
    Khodabandeh, A.
    PROCEEDINGS OF THE 28TH INTERNATIONAL TECHNICAL MEETING OF THE SATELLITE DIVISION OF THE INSTITUTE OF NAVIGATION (ION GNSS+ 2015), 2015, : 2643 - 2653
  • [6] Array-Aided Single-Frequency State-Space RTK with Combined GPS, Galileo, IRNSS, and QZSS L5/E5a Observations
    Li, Wei
    Nadarajah, Nandakumaran
    Teunissen, Peter J. G.
    Khodabandeh, Amir
    Chai, Yanju
    JOURNAL OF SURVEYING ENGINEERING, 2017, 143 (04)
  • [8] Instantaneous GPS/BeiDou/Galileo Attitude Determination: A Single-Frequency Robustness Analysis under Constrained Environments
    Nadarajah, N.
    Teunissen, P. J. G.
    PROCEEDINGS OF THE ION 2013 PACIFIC PNT MEETING, 2013, : 1088 - 1103
  • [9] Performance analysis and improved method for single epoch, single frequency attitude determination using GPS
    Qin, Hong-Lei
    Chen, Wan-Tong
    Jin, Tian
    Cong, Li
    Jiefangjun Ligong Daxue Xuebao/Journal of PLA University of Science and Technology (Natural Science Edition), 2011, 12 (05): : 431 - 435
  • [10] Reversion from L1-L5 Dual to L5 Single Frequency WAAS in the Presence of RF Interference
    Jan, Shau-Shiun
    Walter, Todd
    Enge, Per
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2010, 46 (03) : 1110 - 1126