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Solar wind dispersion quantity measuring method and device, electronic equipment and medium

A measurement method and technology of dispersion quantity, applied in the field of deep space exploration, which can solve the problems of single downlink signal frequency, narrow bandwidth, and limitation of solar wind observation.

Active Publication Date: 2019-10-18
NAT ASTRONOMICAL OBSERVATORIES CHINESE ACAD OF SCI
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Problems solved by technology

[0003] The traditional method of observing the solar wind using ordinary radio sources, because the signal has no phase information, can only measure intensity scintillation, and cannot directly measure group delay and dispersion. When the angle between the sun-earth-radio source is relatively large The phenomenon of saturation will also appear in the hour, so this method is not suitable for the observation of the perihelion
Although the downlink signals of deep space probes can be used to observe time delay, phase scintillation (Doppler scintillation) and spectrum expansion, etc., but because there are very few deep space probes, and the downlink signal frequency is single (currently mainly concentrated in the X frequency band) , The bandwidth is narrow, and the observation of the solar wind is very limited

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  • Solar wind dispersion quantity measuring method and device, electronic equipment and medium
  • Solar wind dispersion quantity measuring method and device, electronic equipment and medium
  • Solar wind dispersion quantity measuring method and device, electronic equipment and medium

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Embodiment Construction

[0051] Hereinafter, embodiments of the present disclosure will be described with reference to the drawings. It should be understood, however, that these descriptions are exemplary only, and are not intended to limit the scope of the present disclosure. In the following detailed description, for purposes of explanation, numerous specific details are set forth in order to provide a thorough understanding of the embodiments of the present disclosure. It may be evident, however, that one or more embodiments may be practiced without these specific details. Also, in the following description, descriptions of well-known structures and techniques are omitted to avoid unnecessarily obscuring the concept of the present disclosure.

[0052] The terminology used herein is for the purpose of describing particular embodiments only, and is not intended to be limiting of the present disclosure. The terms "comprising", "comprising", etc. used herein indicate the presence of stated features, ...

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Abstract

A solar wind dispersion quantity measuring method based on pulsar signals is applied to the technical field of deep space exploration and comprises the following steps: S1, selecting a pulsar with known standard dispersion quantity for observation according to the position of the sun; S2, receiving a pulsar signal after superposition of solar wind dispersion; S3, searching the current dispersion quantity of the signal; and S4, calculating the dispersion quantity of the solar wind according to the standard dispersion quantity and the current dispersion quantity of the signal. The invention further provides a solar wind dispersion quantity measuring device, electronic equipment and a medium. By measuring the dispersion quantity of the pulsar signal and inverting the dispersion quantity of the pulsar signal according to the characteristics of the solar wind, the near-distance solar wind dispersion quantity measurement of the sun is realized.

Description

technical field [0001] The present disclosure relates to the technical field of deep space exploration, and in particular to a method, device, electronic equipment and medium for measuring solar wind dispersion based on pulsar signals. Background technique [0002] With the successful implementation of the lunar exploration project, my country's deep space exploration has begun. Affected by solar activities such as the solar wind and the corona, the wireless communication environment in deep space is very complicated. A large number of irregularly charged particles in the solar wind will cause radio signals to flicker. Especially during the SCO period, the earth, the sun, and the deep space probe are roughly on the same straight line. When the sun-earth-probe angle (SEP) is small or when the sun is in an active cycle, the deep space Null detectors may experience intermittent or even complete loss of communication. The influence of the solar wind on radio signals also refle...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01R29/08G01J3/00
CPCG01J3/00G01J2003/006G01R29/0814
Inventor 孔德庆李春来张洪波苏彦朱新颖李俊铎邢树果武宇翔
Owner NAT ASTRONOMICAL OBSERVATORIES CHINESE ACAD OF SCI