Method for building satellite navigation system test verification and test assessment mathematic model

A satellite navigation system and mathematical model technology, applied in the fields of electrical digital data processing, special data processing applications, instruments, etc., can solve the problems of satellite navigation system test verification and test evaluation that have not yet established a perfect mathematical model system

Active Publication Date: 2017-12-01
NAT UNIV OF DEFENSE TECH
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Problems solved by technology

Therefore, a complete and clear mathematical model system has not yet been est

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  • Method for building satellite navigation system test verification and test assessment mathematic model
  • Method for building satellite navigation system test verification and test assessment mathematic model
  • Method for building satellite navigation system test verification and test assessment mathematic model

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Embodiment Construction

[0037] The present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0038] The satellite navigation system mathematical model system among the present invention can be expressed as following set structure:

[0039] S=

[0040] Among them, F is the function of the mathematical model system; M is the mathematical model in the mathematical model system; R is the construction criterion of the mathematical model system. Their meanings are as follows:

[0041] 1. Function F of the mathematical model system;

[0042] F embodies the requirements met by the mathematical model system, is the basis for the construction of the mathematical model system, and illustrates the necessity of the existence of the mathematical model system.

[0043] 2. Mathematical model M;

[0044] M is the individual that makes up the mathematical model system. The mathematical model of the satellite navigation system uses mathematic...

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Abstract

The invention discloses a method for building a satellite navigation system test verification and test assessment mathematic model. The method comprises the steps of S1: driven by function and performance verification/assessment of verification, design, construction and application stages of a satellite navigation system, determining a verification/test and assessment project of the satellite navigation system, and forming a verification/test and assessment method for a to-be-tested item; S2: according to driving data, determining a satellite navigation physical system or entity generating the driving data; performing abstraction on a satellite navigation physical system entity/function to form a system level simulation model, wherein the model is a basis of a satellite navigation system test verification and test assessment mathematic model system; and S3: after a satellite navigation system verification/test and assessment model and the system level simulation model are built, performing self-closing verification, and performing abstraction on self-closing verification item and method to form a self-closing verification model. The method has the advantages of simple principle, easy realization, good effect and the like.

Description

technical field [0001] The present invention mainly relates to the field of satellite navigation systems, in particular to a method for establishing a mathematical model for satellite navigation system test verification and test evaluation, mainly to solve the problem of global navigation satellite system (Global Navigation Satellite System, GNSS) in the construction and maintenance phases of the system. The main business, information interface, simulation test and evaluation of key stand-alone machines can also be used to build a satellite navigation ground test system. Background technique [0002] The satellite navigation system is generally composed of three parts: the space segment, the ground segment and the user segment, and its construction is a long-term and complex system engineering. During the construction of the satellite navigation system, in order to verify the new technical system and shorten the joint debugging and testing cycle of the ground operation contr...

Claims

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Application Information

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IPC IPC(8): G06F17/50
CPCG06F30/15G06F30/20
Inventor 黄文德杨俊张利云胡梅陈建云周一帆孙乐园
Owner NAT UNIV OF DEFENSE TECH
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