Determination method of carrier phase integer ambiguity in satellite navigation

A whole-cycle ambiguity, carrier phase technology, applied in satellite radio beacon positioning systems, radio wave measurement systems, measurement devices, etc., can solve optimal ambiguity errors, model errors are insensitive, and cannot detect model errors, etc. problem, to achieve the effect of suppressing ambiguity misjudgment and missed judgment, and suppressing external model error response too sensitive

Active Publication Date: 2017-06-20
CHENGDU GUOXING COMM
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Problems solved by technology

In the prior art, the widely used F-Ratio test mainly depends on the accuracy of the initial ambiguity, which can only detect the error inside the observation equation, but cannot detect the model error outside the observation equation, and is not sensitive to the model error; when the measurement In the presence of unmodeled systematic errors, the accuracy of the estimated parameters does not always reflect their accuracy, so it is very likely that the best ambiguity obtained will be wrong, which is intolerable in high-precision positioning and orientation

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  • Determination method of carrier phase integer ambiguity in satellite navigation
  • Determination method of carrier phase integer ambiguity in satellite navigation
  • Determination method of carrier phase integer ambiguity in satellite navigation

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[0023] The technical solution of the present invention will be further described in detail below in conjunction with the accompanying drawings, but the protection scope of the present invention is not limited to the following description.

[0024] Such as figure 1 As shown, the determination method of the carrier phase integer ambiguity in satellite navigation comprises the following steps:

[0025] S1: Initialization of ambiguity, calculate and solve the floating-point solution and variance-covariance matrix of the integer ambiguity from the double-difference observation equation;

[0026] S2: Search for the ambiguity of the whole circle, and search for the integer ambiguity value with the smallest mean square residual error and the integer ambiguity value with the second smallest mean square residual error;

[0027] S3: Determine the integer ambiguity.

[0028] The step of determining the integer ambiguity includes the following sub-steps:

[0029] S301: Calculate the F v...

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Abstract

The invention discloses a method for determining carrier phase integer ambiguity in satellite navigation. The method for determining the carrier phase integer ambiguity comprises the steps that firstly, the F value checked through F-Ratio and the W value checked through W-Ratio are calculated, the F value checked through F-Ratio is calculated according to the formula shown in the specification, and the W value checked through W-Ratio is calculated according to the formula shown in the specification, wherein according to the relational expressions shown in the specification, is the floating point solution of ambiguity, is the variance-covariance matrix of the ambiguity, is the searched integer ambiguity value with the minimum mean square residual error, is the second integer ambiguity value, L is the double-difference observation quantity, P is the weight matrix, A is the direction matrix, is the pseudorange difference solution, and m is the dimensionality of the double-difference observation quantity; secondly, the worked out F value and the worked out W value are compared with the corresponding threshold values respectively, and therefore the effectiveness of the ambiguity is judged. The ambiguity misjudgment and judgment omission caused by the inner and outer error of a model can be effectively restrained, the ambiguity resolving success rate can be effectively improved, the ambiguity fixing time can be shortened, and the system can obtain a high-precision positioning and orienting result easily.

Description

technical field [0001] The invention relates to a method for determining the integer ambiguity of carrier phase in satellite navigation. Background technique [0002] With the development of science and technology, the application of satellite navigation is becoming more and more extensive. In a satellite navigation system, we can usually obtain two basic observations from satellite signals, which are pseudorange and carrier phase. Carrier phase observations are much more accurate than pseudoranges, so they are high-precision positioning and orientation basic method. However, there is ambiguity in carrier phase measurement, and ambiguity is an unknown fixed preconceived value. Once the ambiguity of the whole circle is fixed, the carrier phase can be used as an accurate pseudo-range measurement without ambiguity, so the resolution and determination of ambiguity become a crucial aspect in high-precision positioning and orientation. [0003] The ambiguity resolution is usual...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01S19/44
CPCG01S19/44
Inventor 廖国军
Owner CHENGDU GUOXING COMM
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