Satellite position and speed forecasting method based on GLONASS almanac parameters
A satellite position and parameter technology, applied in the field of satellite position and velocity prediction based on GLONASS almanac parameters, can solve problems such as complex expressions and many calculation steps
Patent Information
- Authority / Receiving Office
- CN · China
- Current Assignee / Owner
- Publication Date
- 2017-10-10
- Estimated Expiration
- Not applicable · inactive patent
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Abstract
Description
technical field
[0001] The invention relates to the technical field of satellite navigation, in particular to a satellite position and speed prediction method based on GLONASS almanac parameters. Background technique
[0002] The almanac parameter is an important part of the navigation message of the satellite navigation system, and it plays a very important role in the signal acquisition process of the navigation receiver. In the absence of auxiliary information, the receiver estimates the approximate position and velocity of the satellite based on the almanac parameters, reproduces the visible satellite and searches for it, avoiding searching for satellites in the sky. At the same time, the approximate Doppler frequency shift of the satellite relative to the receiver is estimated according to the satellite speed, which can assist in the frequency domain search signal during the signal acquisition stage, greatly shortening the satellite signal acquisition time, thereby shor...
Examples
Embodiment Construction
[0044] Examples are given below to describe the present invention in detail.
[0045] Based on the special definition of GLONASS almanac parameters, the present invention improves the existing classical GPS user algorithm model in a targeted manner, and provides a satellite position and speed prediction method based on GLONASS almanac parameters, based on the principle of satellite orbit dynamics and satellite position The method of expressing the orbital elements of the velocity, according to the GLONASS almanac parameters (as shown in Table 1), calculate the orbital parameters such as the average angular velocity, the semi-major axis, the deviating anomaly angle, the mean anomaly angle, and the right ascension of the ascending node and their changes at the observation time Rate, and then obtain the latitude angle, latitude angle change rate, radial vector and radial vector change rate at the observation time, from which the position and speed of the satellite in the orbital c...