Dual-satellite positioning method based on WGS (World Geodetic System)-84 model

A WGS-84, positioning method technology, applied in satellite radio beacon positioning systems, measuring devices, instruments, etc., can solve problems such as positioning solution ambiguity, inability to uniformly solve satellite co-orbit/different orbit, and iterative methods to solve problems such as difficulty

Active Publication Date: 2018-06-29
UNIV OF ELECTRONICS SCI & TECH OF CHINA
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Problems solved by technology

[0003] At present, the positioning method of joint time difference / frequency difference in dual-satellite positioning cannot uniformly solve the situation of satellite co-orbit / difference when using the analytical method for positioning; using the Newton iteration method depends on the initial value point of the target, and the calculation amount is large. The stability of the algorithm is not good, and there is a problem of positioning and defuzzification
For double-star direction finding and positioning, there are also problems such as the high degree of nonlinearity of the direction finding equation and the difficulty in solving iterative methods.

Method used

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  • Dual-satellite positioning method based on WGS (World Geodetic System)-84 model

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Embodiment Construction

[0088] The following is a verification and description of the above-mentioned closed solution algorithm scheme for direction finding and positioning based on the WGS-84 earth ellipsoid model constrained by the accompanying drawings. First, the following reasonable assumptions are made for the system model:

[0089] 1. Assume that the double star is a low-orbit satellite, and the orbital height is relatively low, usually 500km to 1000km;

[0090] 2. Unify the satellite attitude measurement error existing in engineering practice into the satellite direction finding error;

[0091] 3. Assume that the measurement errors obey a Gaussian distribution with a mean of zero, and the errors are independent of each other.

[0092] (1) Positioning effect when double stars are in different orbits:

[0093] Such as figure 2 As shown, it is assumed that the binary star is an out-of-orbit binary star, and the orbit heights are H S1 =500km,H S2 =550km, the corresponding satellite sub-satel...

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Abstract

The invention belongs to the technical field of electronic countermeasures, in particular to a dual-satellite positioning method based on a WGS (World Geodetic System)-84 model. A dual-satellite direction-finding positioning closed resolving method based on the WGS-84 model is provided, the dual-satellite direction-finding closed resolving method is provided through the pseudo linearization of anangle measuring equation and combination of WGS-84 earth ellipsoidal model restraint, earth surface target radiation source is positioned and resolved, a weighted least square solution analysis of thetarget under the restraining action of an earth ellipsoidal model is provided; as proved by the simulation, the algorithm can approach the Cramer-Rao low bound (CRLB) of positioning error when the system direction-finding error is not very large; compared with the conventional method of directly resolving a multivariate non-linear equation by an analytical method and using a Newton iteration method to resolve the target position, the method has the advantages that when the two satellites are in the same rail or different rails, the target can be positioned and resolved uniformly, under the method, the configuration of a satellite is flexible, iteration resolution is not required, calculation amount is low, and the problem of inaccurate positioning solution is solved.

Description

technical field [0001] The invention belongs to the technical field of electronic countermeasures, and in particular relates to a double-star positioning method based on the WGS-84 model. Background technique [0002] With the militarization of space and the rapid development of electronic reconnaissance satellites, space has gradually become the strategic commanding heights for safeguarding national security and interests. The satellite-based space electronic reconnaissance system is not affected by space due to its wide-area coverage and little influence of climate factors. The characteristics of geographical restrictions have attracted widespread attention from the military of various countries, and the use of satellite reconnaissance systems to obtain information has become an important source of intelligence for battlefield operations. At present, my country's aerospace industry is developing rapidly, and satellite detection technology has been rapidly developed and wid...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01S19/46
CPCG01S19/46
Inventor 李万春陈锐滨扶彩霞王敏郭昱宁
Owner UNIV OF ELECTRONICS SCI & TECH OF CHINA
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