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Patent

Rapid visible satellite selection method based on multimode GNSS receiver

TLDR
In this paper, a rapid visible satellite selection method based on a multimode GNSS receiver is proposed, which comprises the steps that (1) elevation angles, received by the multimode GPS receiver currently, of all visible satellites are calculated, the satellites with the satellite elevation angles smaller than 10 degrees are eliminated, and a usable visible satellite set S is obtained; (2) according to satellite position information of the satellites and receiver preliminary position information, a coefficient matrix and a weight coefficient matrix are calculated; (3) a GDOP value corresponding to S is calculated, a contribution
Abstract
The invention discloses a rapid visible satellite selection method based on a multimode GNSS receiver. The method comprises the steps that (1) elevation angles, received by the multimode GNSS receiver currently, of all visible satellites are calculated, the satellites with the satellite elevation angles smaller than 10 degrees are eliminated, and a usable visible satellite set S is obtained; (2) according to satellite position information of the satellites and receiver preliminary position information, a coefficient matrix and a weight coefficient matrix are calculated; (3) a GDOP value corresponding to the visible satellite set S is calculated; (4) a contribution value delta Gi of each visible satellite to GDOP is calculated and the contribution values delta Gi are ranked from large to small, so that a set SG is formed; (5) when the multimode GNSS receiver needs to select N visible satellites for navigation and location, the front N satellites in the set SG are selected, and a corresponding visible satellite subset is a selected usable satellite constellation. The method has the advantages of being convenient and quick to operate, simple in implementation, high in accuracy, wide in application range and the like.

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Citations
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Patent

Rapid satellite selection method for Beidou satellite navigation system

Ding Zihan, +1 more
TL;DR: In this paper, the authors proposed a rapid satellite selection method for a Beidou satellite navigation system, which considers the special situation of geometric distribution of satellite space and considers the influence on satellite selection results of various complex situations.
Patent

Beidou navigation constellation rapid satellite selection method

Ding Zihan
TL;DR: In this article, a Beidou navigation constellation rapid satellite selection method, belonging to the satellite navigation field, is presented, where the discrete Hopfield neural network algorithm is employed to perform GDOP (Geometric Dilution of Precision) calculation formula optimization so as to avoid the matrix inversion operation in the traditional GDOP calculation, reduce the calculation amount of the GDOP solution and satisfy the user's requirements for accuracy, timeliness and robustness of the satellite positioning.
Patent

Satellite selection method used for navigation of single-system and multi-system satellite combination

TL;DR: In this paper, a satellite selection method used for navigation of a single-system and multi-system satellite combination is presented. But the method comprises steps of dividing constellations according to systems participating in the positioning; according to the inclination angles of visible satellites in each constellation, naming the region whose value is lower than a certain inclination angle threshold as the low-inclination angle region; successively selecting satellites with the biggest inclination angle and the second big inclination angel as the fifth and sixth satellites from rest visible satellites, and finally, calculating GDOPs of all satellite combinations
Patent

Beidou satellite selection method based on satellite signal energy and spatial orientation information

TL;DR: In this article, the authors proposed a satellite selection method based on satellite signal energy and spatial orientation information, and solved the problem of satellite selection under extreme conditionsthat a shielding object exists and the like.
Patent

Quick satellite selection method for satellite navigation receiver

TL;DR: In this paper, a quick satellite selection method for a satellite navigation receiver is proposed, which comprises steps: the approximate position of a satellite is calculated, a constellation is pre-selected, a contribution value is calculated and ranking is carried out according to the contribution values of geometric precision factors, navigation satellites with small contribution values are eliminated one by one from small to large until the remaining navigation satellite number meets the requirement of the minimum navigation satellite numbers needed for positioning and calculation.
References
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Patent

A signal receiving method for a user's device in a global positioning system

TL;DR: In this paper, the authors propose a frequency of executing the positioning for a GPS device that is almost as equal as conventionally, whereby the load of a microprocessor in the user's device can be remarkably reduced.
Patent

Satellite positioning apparatus and current position determining method

TL;DR: In this paper, the available-satellite record data is extracted from a GPS receiver and four candidate satellites are selected so that the satellites used for satellite positioning the previous time are selected with priority as the satellites to be used for positioning this time, and the selected satellites are set in designated satellite data.
Patent

Satellite selection method and satellite navigation positioning method applying the satellite selection method

TL;DR: In this article, a satellite selection method and a satellite navigation positioning method applying the satellite selection algorithm are presented. But the satellite positioning method is not applied in this paper, instead, it is used for satellite selection.