CLC number: TP39; V19
On-line Access: 2024-08-27
Received: 2023-10-17
Revision Accepted: 2024-05-08
Crosschecked: 2019-06-11
Cited: 0
Clicked: 6644
Citations: Bibtex RefMan EndNote GB/T7714
Qiao Wang, Xiao-Jun Jin, Wei Zhang, Shi-Ming Mo, Zhao-Bin Xu, Zhong-He Jin. An online error calibration method for spaceflight TT&C systems based on LEO-ground DDGPS[J]. Frontiers of Information Technology & Electronic Engineering, 2019, 20(6): 829-841.
@article{title="An online error calibration method for spaceflight TT&C systems based on LEO-ground DDGPS",
author="Qiao Wang, Xiao-Jun Jin, Wei Zhang, Shi-Ming Mo, Zhao-Bin Xu, Zhong-He Jin",
journal="Frontiers of Information Technology & Electronic Engineering",
volume="20",
number="6",
pages="829-841",
year="2019",
publisher="Zhejiang University Press & Springer",
doi="10.1631/FITEE.1800308"
}
%0 Journal Article
%T An online error calibration method for spaceflight TT&C systems based on LEO-ground DDGPS
%A Qiao Wang
%A Xiao-Jun Jin
%A Wei Zhang
%A Shi-Ming Mo
%A Zhao-Bin Xu
%A Zhong-He Jin
%J Frontiers of Information Technology & Electronic Engineering
%V 20
%N 6
%P 829-841
%@ 2095-9184
%D 2019
%I Zhejiang University Press & Springer
%DOI 10.1631/FITEE.1800308
TY - JOUR
T1 - An online error calibration method for spaceflight TT&C systems based on LEO-ground DDGPS
A1 - Qiao Wang
A1 - Xiao-Jun Jin
A1 - Wei Zhang
A1 - Shi-Ming Mo
A1 - Zhao-Bin Xu
A1 - Zhong-He Jin
J0 - Frontiers of Information Technology & Electronic Engineering
VL - 20
IS - 6
SP - 829
EP - 841
%@ 2095-9184
Y1 - 2019
PB - Zhejiang University Press & Springer
ER -
DOI - 10.1631/FITEE.1800308
Abstract: To overcome the shortcomings of the traditional measurement error calibration methods for spaceflight telemetry, tracking and command (TT&C) systems, an online error calibration method based on low Earth orbit satellite-to-ground double- differential GPS (LEO-ground DDGPS) is proposed in this study. A fixed-interval smoother combined with a pair of forward and backward adaptive robust Kalman filters (ARKFs) is adopted to solve the LEO-ground baseline, and the ant colony optimization (ACO) algorithm is used to deal with the ambiguity resolution problem. The precise baseline solution of DDGPS is then used as a comparative reference to calibrate the systematic errors in the TT&C measurements, in which the parameters of the range error model are solved by a batch least squares algorithm. To validate the performance of the new online error calibration method, a hardware-in-the-loop simulation platform is constructed with independently developed spaceborne dual-frequency GPS receivers and a Spirent GPS signal generator. The simulation results show that with the fixed-interval smoother, a baseline estimation accuracy (RMS, single axis) of better than 10 cm is achieved. Using this DDGPS solution as the reference, the systematic error of the TT&C ranging system is effectively calibrated, and the residual systematic error is less than 5 cm.
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