Beidou broadcast ephemeris maneuvering fault monitoring method considering parameter sensitivity

A technology for broadcast ephemeris and fault monitoring, applied in the field of satellite navigation, can solve the problems of high observation noise and complex ambiguity solution, achieve the effect of high observation accuracy and reduce the complexity of solution

Active Publication Date: 2021-01-08
HARBIN ENG UNIV
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Problems solved by technology

[0005] In order to solve the problems of large observation noise or complex ambiguity resolution in the Beidou broadcast ephemeris maneuver fault monitoring of pseudorange and carrier phase observations, the present invention provides a Beidou broadcast ephemeris maneuver fault monitoring considering parameter sensitivity Method, the orbit error is measured by combining pseudorange and carrier phase observations, combined with the sensitivity analysis of satellite position error to the change of broadcast ephemeris parameters, the observation equation is constructed, and the minimum detectable error (Minimum Detectable Error) is calculated according to the integrity risk requirements of the system. Error, MDE), choosing a reasonable MDE detection threshold can realize Beidou broadcast ephemeris mobile fault monitoring

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  • Beidou broadcast ephemeris maneuvering fault monitoring method considering parameter sensitivity
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  • Beidou broadcast ephemeris maneuvering fault monitoring method considering parameter sensitivity

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Embodiment

[0019] The present invention is a Beidou broadcast ephemeris mobile fault monitoring method in consideration of parameter sensitivity, and the specific steps include:

[0020] Step 1. Sensitivity analysis of satellite position error to broadcast ephemeris parameter changes

[0021] The positions of Beidou geostationary orbit satellites, inclined geosynchronous orbit satellites, and medium-circle earth orbit satellites can be calculated by using the satellite position nonlinear function defined in the Beidou Interface Control Document-2013. The sensitivity coefficient of the satellite position to the change of the broadcast ephemeris parameters can be calculated by the differential calculation of each broadcast ephemeris parameter by the satellite position function, the formula is as follows

[0022]

[0023] Among them, A is a sensitivity matrix of 3×15, x, y, z are calculation functions of satellite positions, P is a matrix containing 15 broadcast ephemeris parameters, t ...

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Abstract

The invention relates to a Beidou broadcast ephemeris maneuvering fault monitoring method considering parameter sensitivity, and belongs to the technical field of satellite navigation. The method specifically comprises the following steps of: 1, analyzing the sensitivity of satellite position errors to broadcast ephemeris parameter changes; and 2, measuring the orbit error in the sight distance direction of the satellite by adopting pseudo-range difference, measuring the orbit error orthogonal to the sight distance direction by adopting double-difference carrier phase, and constructing an observation equation about the position error of the satellite. According to the method, the orbit error is measured in a pseudo-range and carrier phase observed quantity combined mode, sensitivity analysis of the satellite position error on broadcast ephemeris parameter changes is fully utilized, an observation equation related to the satellite position error is converted into an observation equationrelated to broadcast ephemeris parameter deviation, higher observation precision is obtained, the ambiguity resolving complexity in carrier phase observation is reduced, a monitoring model can be built, and Beidou broadcast ephemeris maneuvering type fault monitoring can be achieved.

Description

technical field [0001] The invention relates to a Beidou broadcast ephemeris mobile fault monitoring method in consideration of parameter sensitivity, and belongs to the technical field of satellite navigation. Background technique [0002] With the development of satellite navigation system, applying it to aircraft precision approach service can effectively improve flight safety and efficiency. Among them, satellite broadcast ephemeris failure is one of the main risk sources affecting aircraft precision approach. In order to ensure the integrity of the user's positioning, the monitoring of broadcast ephemeris faults is essential. [0003] Broadcast ephemeris faults can be divided into maneuvering faults and non-maneuvering faults. Non-maneuvering faults can be effectively monitored by the method of predicting ephemeris minus today's ephemeris. For the detection of maneuvering faults, the receiver autonomous integrity monitoring algorithm (Receiver Autonomous Integrity Mo...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01S19/20
CPCG01S19/20
Inventor 李慧刘媛媛冯伟男李梦浩李南李亮
Owner HARBIN ENG UNIV
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