A method is described for joint precise point positioning and attitude determination with tight coupling of two single-frequency low-cost global navigation satellite system receivers and an inertial sensor. The sensor fusion is performed with an extended Kalman filter. The carrier phase ambiguities are determined in a constrained tree search using soft a priori information on the antenna distance. A code multipath parameter is determined for each satellite to improve the accuracy. Ionospheric corrections are estimated also by single-frequency receivers.
Tightly coupled precise point positioning and attitude determination
IEEE Transactions on Aerospace and Electronic Systems ; 51 , 4 ; 3182-3197
2015-10-01
8315855 byte
Article (Journal)
Electronic Resource
English
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