Space debris orbit determination traversal observation method and system

A space debris and orbit determination technology, which is applied in the aerospace field, can solve the problems of improving the orbit determination accuracy of single satellite observation data of a single type of payload, and achieve the effect of improving the orbit determination accuracy.

Pending Publication Date: 2020-09-01
INNOVATION ACAD FOR MICROSATELLITES OF CAS +1
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Problems solved by technology

[0005] However, these methods mainly achieve the improvement of orbit determination accuracy through multi-source data fusion processing or the use of multi-satellite sys...

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  • Space debris orbit determination traversal observation method and system
  • Space debris orbit determination traversal observation method and system
  • Space debris orbit determination traversal observation method and system

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[0023] In the following description, the present invention is described with reference to various examples. One skilled in the art will recognize, however, that the various embodiments may be practiced without one or more of the specific details, or with other alternative and / or additional methods, materials, or components. In other instances, well-known structures, materials, or operations are not shown or described in detail so as not to obscure the inventive concepts of the present invention. Similarly, for purposes of explanation, specific quantities, materials and configurations are set forth in order to provide a thorough understanding of embodiments of the invention. However, the invention is not limited to these specific details. Furthermore, it should be understood that the embodiments shown in the drawings are illustrative representations and are not necessarily drawn to correct scale.

[0024] In this specification, reference to "one embodiment" or "the embodiment...

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Abstract

The invention discloses a space debris orbit determination traversal observation method and system. A camera installed in a +Y-axis direction of a satellite arranged on a terminator sun synchronous orbit is controlled to rotate around a +Z axis; large-range scanning from a starting deflection angle to an ending deflection angle is achieved, then space debris orbit determination traversal observation of the synchronous belt is achieved; and in the observation process, through real-time calculation, the rotating angle of a satellite around the +X axis of a satellite body is controlled to ensurethat the visual axis of a camera is always perpendicular to the geosynchronous belt at the specified latitude.

Description

technical field [0001] The invention relates to the field of aerospace technology, in particular to a space debris orbit determination and traversal observation method. Background technique [0002] At present, the number of various space vehicles and debris has increased significantly, and space activities have become increasingly frequent, posing a serious threat to satellite safety, especially the geosynchronous belt is the gathering place for many communication, broadcasting, meteorological, early warning and military reconnaissance satellites. Therefore, space debris in the synchronous belt Observation is becoming more and more important. [0003] Space debris observation includes ground-based and space-based methods. Compared with ground-based observation, space-based space debris observation has higher quota coverage and observation timeliness. However, limited by the limitation of sensor capabilities and the constraints of orbital periodicity, the observation arcs o...

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Application Information

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IPC IPC(8): G01C21/24G01S19/25
CPCG01C21/24G01S19/258
Inventor 陈起行胡海鹰朱永生郑珍珍董磊盛蕾王威
Owner INNOVATION ACAD FOR MICROSATELLITES OF CAS
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