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Moon detector, moon detector combination full space measurement and control apparatus, and measurement and control method of moon detector combination full space measurement and control apparatus

A technology of measurement and control devices and detectors, applied to radio transmission systems, electrical components, transmission systems, etc., can solve problems such as the inability to realize full-space measurement, achieve optimal layout, increase microwave networks, and realize the connection of high-frequency signals Effect

Inactive Publication Date: 2017-05-10
SHANGHAI AEROSPACE SYST ENG INST
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  • Application Information

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Problems solved by technology

[0003] The problem solved by the present invention is that in the prior art, when the beam of the lunar probe is blocked by the solar sail, the full-space measurement cannot be realized; in order to solve the above problem, the present invention provides a full-space measurement and control device for the lunar probe and its combination and measurement and control methods

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Embodiment Construction

[0021] The present invention will be further elaborated below in conjunction with the accompanying drawings and specific embodiments. It should be noted that the drawings are all in a very simplified form and use imprecise ratios, which are only used to facilitate and clearly assist the purpose of illustrating the embodiments of the present invention.

[0022] figure 1 It is a schematic structural diagram of the full-space measurement and control device of the lunar probe assembly provided by the embodiment of the present invention, Figure II It is a schematic diagram of antenna installation for the full-space measurement and control device of the lunar probe assembly provided by the embodiment of the present invention. combined reference figure 1 and figure 2 , The lunar probe assembly full-space measurement and control device provided by the present invention includes: the first receiving antenna 109, the transponder a101, the fixed place a102, and the first transmittin...

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Abstract

The invention provides a moon detector, a moon detector combination full space measurement and control apparatus, and a measurement and control method of the moon detector combination full space measurement and control apparatus. The moon detector undertakes complicated tasks, so the moon detector is usually formed by multiple independent sub-detectors, each sub-detector needs to be equipped with an independent measurement and control communication system, and the systems are used for independent communication between the sub-detectors and the earth and also for communication among the sub-detectors. In this way, each sub-detector needs to be independently equipped with a measurement and control antenna, and wave beams of the measurement and control antennas need to cover the whole space. However, for the complicated moon detector in a combination state, the detector is large in size if solar panels of the detector are unfolded and the wave beams of the measurement and control antennas are blocked, so it is difficult to guarantee that the measurement and control antennas of the moon detector in the combination state can realize full space wave beam coverage. To realize full space wave beam coverage of the measurement and control antennas, the invention provides the moon detector, the moon detector combination full space measurement and control apparatus, and the measurement and control method of the moon detector combination full space measurement and control apparatus.

Description

technical field [0001] The invention relates to a full-space detection scheme of a lunar probe, in particular to a full-space measurement and control device and a measurement and control method for a lunar probe and its assembly when the measurement and control antenna beam is blocked by a solar sail. Background technique [0002] In the current measurement and control scheme of the lunar probe, there is generally no situation where the solar panel blocks the beam of the measurement and control antenna, so the traditional measurement and control scheme cannot be applied to the situation where the solar panel blocks the beam. In the face of solar panels blocking the beam, the attitude is generally adjusted to ensure that the antenna beam can point to the earth. However, this solution cannot guarantee full-space measurement and control, and the reliability of measurement and control is low. If the earth enters an area covered by solar panels, the measurement and control commun...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H04B1/40H04B7/185
Inventor 江炜刘江澜施飞舟李天义侯建文闫虎新魏然
Owner SHANGHAI AEROSPACE SYST ENG INST
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