Ranging code correlation integral improvement method for satellite navigation
A correlation integration and satellite navigation technology, applied in the field of satellite navigation, can solve problems such as affecting the accuracy of pseudorange measurement and difficult to maintain symmetry of pseudocode correlation functions.
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[0062] The present invention will be further described below in conjunction with the accompanying drawings.
[0063] In order to analyze the correlation integral model of the ranging code more specifically, the phase of the ranging code is expanded by Taylor, the carrier phase is not expanded, and the received signal can be expressed as
[0064]
[0065] For recurring signals, it can be expressed as:
[0066]
[0067] In the formula, n 0 , R CO , Respectively for a relevant integration period T I The initial value of the ranging code phase of the received signal and its first, second and third order derivatives, ε nr (kT S ) is the remainder error of the ranging code phase Taylor expansion of the received signal, T S is the system sampling frequency, c( ) is the ranging code data, exp( ) is the complex form of the carrier, φ 0 (kT S ) means relative to the integration period T I The carrier phase of the kth sampling point within; n, R C , and are the initi...
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