Satellite navigation fast positioning method and device and satellite navigation receiver
A technology of satellite navigation and positioning method, which is applied in the field of satellite navigation to achieve fast convergence speed, reduce ill-conditionedness, and improve the accuracy and speed of solution
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Embodiment 1
[0030] see figure 1 , is the satellite navigation fast positioning method provided by Embodiment 1 of the present invention. It should be noted that if there are substantially the same results, the satellite navigation fast positioning method of the present invention does not use figure 1 The flow sequence shown is limited. The method comprises the steps of:
[0031] S101. During the satellite navigation rapid positioning process, determine whether the observation equation is ill-conditioned.
[0032] In Embodiment 1 of the present invention, S101 may specifically include the following steps:
[0033] S1011. Receive the satellite signal and the differential data of the satellite navigation receiver of the reference station according to the epoch, decode the satellite signal and the differential data, and respectively obtain the relative distances of the target satellite navigation receiver and the satellite navigation receiver of the reference station in each epoch data obs...
Embodiment 2
[0086] see Figure 4 , the present invention provides a satellite navigation fast positioning device, said device comprising:
[0087] Judgment module 11, used for judging whether the observation equation is pathological during the fast positioning process of satellite navigation;
[0088] The solving module 12 is used for when the observation equation is ill-conditioned, using an adaptive weighted differential evolution algorithm combined with regularization to solve the ill-conditioned observation equation during fast positioning, and obtaining the real number solution ambiguity component of the vector to be found in the ill-conditioned observation equation;
[0089] The search module 13 is used to use the real ambiguity resolution component of the vector to be sought in the observation equation as an input value, and search for an integer solution of the ambiguity of the vector to be sought in the observation equation;
[0090] The exact coordinate calculation module 14 is...
Embodiment 3
[0092] Embodiment 3 of the present invention also provides a computer-readable storage medium, the computer-readable storage medium stores a computer program, and when the computer program is executed by a processor, the satellite navigation rapid positioning as provided in Embodiment 1 of the present invention is realized. method steps.
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