Manned spacecraft remote test system

A manned spacecraft and remote testing technology, applied in the field of manned spacecraft testing, can solve the problems of large demand and mobility of personnel, frequent switching of work task status, and long-term business trips of testers, so as to achieve efficient remote testing tasks, Improve the level of research and development and reduce the effect of occupation

Inactive Publication Date: 2018-04-06
BEIJING SPACE TECH RES & TEST CENT
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Problems solved by technology

Testers generally work in the test command center. When the spacecraft is running to the final assembly center and launch site for testing, the testers need to travel for a long time
[0005] (2) Constraints on test personnel: In the case of intensive launch of spacecraft, experts face the problem of long-term multi-spacecraft and multi-site parallel work. The demand and mobility of personnel are large, the status of work tasks is switched frequently, and there is a lack of unified command and control. Cooperate with models in multiple places to carry out tests in parallel

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Embodiment Construction

[0027] The description of the embodiments in this specification should be combined with the corresponding drawings, and the drawings should be regarded as a part of the complete specification. In the drawings, the shapes or thicknesses of the embodiments may be exaggerated and marked for simplification or convenience. Furthermore, parts of each structure in the drawings will be described separately. It should be noted that elements not shown in the drawings or described in words are forms known to those of ordinary skill in the art.

[0028] The descriptions of the embodiments here, any references to directions and orientations are just for convenience of description, and should not be construed as any limitation to the protection scope of the present invention. The following descriptions of the preferred embodiments involve combinations of features, which may exist independently or in combination, and the present invention is not particularly limited to the preferred embodime...

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Abstract

The invention relates to a manned spacecraft remote test system. The manned spacecraft remote test system comprises multiple remote test front-end subsystems which are arranged in a manned spacecraftassembly center or a manned spacecraft launch center and used for receiving the field data from the tested manned spacecraft; and a remote test processing and monitoring subsystem which is arranged ina manned spacecraft test command center and communicates with multiple remote test front-end subsystems through a remote network and is used for receiving the field data from multiple remote test front-end subsystems in real time and analyzing and processing the field data. The occupation contradiction of manpower and material resources can be effectively solved so that the launch efficiency canbe enhanced, the launch cost can be reduced and multi-spacecraft and multi-area comprehensive test tasks can be met.

Description

technical field [0001] The invention relates to the technical field of manned spacecraft testing, in particular to a manned spacecraft remote testing system. Background technique [0002] The remote remote collaborative test of manned spacecraft means that the spacecraft under test and the testers and test equipment are in different regions, and the distance between them ranges from a few kilometers to hundreds or thousands of kilometers. And the corresponding data are transmitted through a specific link. [0003] With the mass production of spacecraft models and the further increase of high-density test launch development tasks, there are multi-spacecraft, multi-site, and parallel testing situations, and the traditional spacecraft local test system can no longer meet the requirements. At present, manned spacecraft testing mainly has the following defects: [0004] (1) Test tasks and site constraints: Manned spacecraft will face tests at different locations such as the tes...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01D21/02H04L12/26
CPCG01D21/02H04L43/00
Inventor 何永丛潘顺良杨枫任亮
Owner BEIJING SPACE TECH RES & TEST CENT
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