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Sensors 2017, 17(2), 408; doi:10.3390/s17020408

Formal Uncertainty and Dispersion of Single and Double Difference Models for GNSS-Based Attitude Determination

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Engineering Center of SHMEC for Space Information and GNSS, East China Normal University, Shanghai 200241, China
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Key Laboratory of Geographic Information Science, Ministry of Education, East China Normal University, Shanghai 200241, China
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Shanghai Key Laboratory of Multidimensional Information Processing, East China Normal University, Shanghai 200241, China
*
Author to whom correspondence should be addressed.
Academic Editor: Assefa M. Melesse
Received: 21 November 2016 / Revised: 4 February 2017 / Accepted: 16 February 2017 / Published: 20 February 2017
(This article belongs to the Section Remote Sensors)
View Full-Text   |   Download PDF [7613 KB, uploaded 20 February 2017]   |  

Abstract

With multi-antenna synchronized global navigation satellite system (GNSS) receivers, the single difference (SD) between two antennas is able to eliminate both satellite and receiver clock error, thus it becomes necessary to reconsider the equivalency problem between the SD and double difference (DD) models. In this paper, we quantitatively compared the formal uncertainties and dispersions between multiple SD models and the DD model, and also carried out static and kinematic short baseline experiments. The theoretical and experimental results show that under a non-common clock scheme the SD and DD model are equivalent. Under a common clock scheme, if we estimate stochastic uncalibrated phase delay (UPD) parameters every epoch, this SD model is still equivalent to the DD model, but if we estimate only one UPD parameter for all epochs or take it as a known constant, the SD (here called SD2) and DD models are no longer equivalent. For the vertical component of baseline solutions, the formal uncertainties of the SD2 model are two times smaller than those of the DD model, and the dispersions of the SD2 model are even more than twice smaller than those of the DD model. In addition, to obtain baseline solutions, the SD2 model requires a minimum of three satellites, while the DD model requires a minimum of four satellites, which makes the SD2 more advantageous in attitude determination under sheltered environments. View Full-Text
Keywords: formal uncertainty; dispersion; single difference; double difference; GNSS; common clock formal uncertainty; dispersion; single difference; double difference; GNSS; common clock
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This is an open access article distributed under the Creative Commons Attribution License which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. (CC BY 4.0).

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Chen, W.; Yu, C.; Dong, D.; Cai, M.; Zhou, F.; Wang, Z.; Zhang, L.; Zheng, Z. Formal Uncertainty and Dispersion of Single and Double Difference Models for GNSS-Based Attitude Determination. Sensors 2017, 17, 408.

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