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GEO target multipoint preferred short arc orbit determination method based on space-based optical observation data

An observation data and optical technology, applied in the aerospace field, can solve the problems such as the inability to guarantee the convergence and accuracy of the initial orbit of the short arc, and the short arc of the GEO target observation.

Active Publication Date: 2020-08-18
NO 63921 UNIT OF PLA
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Problems solved by technology

[0003] However, due to the high speed of the satellite platform itself, the observation arc of each GEO target is short, and the convergence and accuracy of the short-arc initial orbit determination cannot be guaranteed.

Method used

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  • GEO target multipoint preferred short arc orbit determination method based on space-based optical observation data
  • GEO target multipoint preferred short arc orbit determination method based on space-based optical observation data
  • GEO target multipoint preferred short arc orbit determination method based on space-based optical observation data

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specific example

[0096] Table 1 Accuracy and success rate of GEO short-arc orbit determination for space-based optical surveillance

[0097]

[0098] The results in Table 1 are based on the common sun-synchronous orbit space-based optical surveillance platform as the simulation scene to patrol and observe 3235 arcs of GEO targets, each observation lasts about 3 minutes, and the observation accuracy of right ascension and declination is about 10 arc seconds . Among them, the success rate of orbit determination is the proportion of the number of successful arcs of the specified orbit. Among them, the failure of orbit determination mainly includes the failure to converge to obtain the number of orbits, the orbit converges to a trivial solution, and the error of the semi-major axis of the orbit is too large (the semi-major axis error is defined in this paper. Long axis error ≥ 1000km), etc. It can be seen from Table 1 that the semi-major axis orbit determination accuracy of the method in this ...

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Abstract

The invention discloses a GEO target multi-point preferred short arc orbit determination method based on space-based optical observation data. The GEO target multi-point preferred short arc orbit determination method is an orbit determination scheme with high robustness and high precision for GEO target short arcs of the space-based optical observation data. The specific technical scheme is as follows, the method comprises the following steps: firstly, carrying out short-arc orbit determination on angle measurement numbers of any two points based on GEO target orbit near-circle hypothesis; andthen carrying out orbit selection by utilizing the residual first-order variation of the observation data sequence, finally converting a plurality of groups of optimized orbit elements into a position vector and a speed vector, and carrying out merging processing to obtain a high-precision and steady GEO target short arc orbit determination result. The scheme is a GEO target high-stability and high-precision short-arc orbit determination method suitable for space-based optical observation data, and can be expanded and applied to the field of short-arc orbit determination of global high-orbitand low-orbit targets by space-based foundation optics and radars.

Description

technical field [0001] The invention relates to the field of spaceflight technology, in particular to a multi-point preferred short-arc orbit determination method for GEO targets based on space-based optical observation data. Background technique [0002] High-orbit satellites, or GEO satellites, have stable ground pointing and condescending large field of view observation conditions. They are widely used in global communications, reconnaissance, early warning and other fields, and are scarce strategic space resources. Ground-based optical telescopes are the backbone equipment for GEO target detection, but limited by the global deployment of ground-based equipment, they cannot effectively detect and monitor GEO targets outside the station deployment area. Space-based optical surveillance satellites have the characteristics of global inspections, and can quickly search and scan or stare at and track multiple GEO targets. If they adopt sun-synchronous orbits or small-inclinati...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C21/24G01C23/00
CPCG01C21/24G01C23/00
Inventor 黄剑张兵苑刚姚刚熊建宁雷祥旭
Owner NO 63921 UNIT OF PLA
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