In-orbit test method for low earth orbit long-life manned spacecraft

A technology of manned spacecraft and testing method, which is applied in the field of on-orbit testing of low-orbit long-life manned spacecraft, and can solve the problems that it is difficult to adapt to the on-orbit mission requirements of manned spacecraft and satellite on-orbit testing methods.

Active Publication Date: 2018-08-17
BEIJING SPACE TECH RES & TEST CENT
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AI Technical Summary

Problems solved by technology

The existing technical means have the following problems: ① Manned spacecraft needs to carry out multiple on-orbit tests during different flight stages, such as platform tests at the initial stage of orbiting, tests before each rendezvous and docking mission, regular The frequency of on-orbit testing is much higher than that of satellites, and the existing satellite on-orbit testing methods are difficult to adapt to and meet the needs of manned spacecraft to carry out multiple on-orbit tests; There are many mission modes and types. If you need to carry out multiple rendezvous and docking missions with manned spacecraft and cargo spacecraft, you need to carry out multiple propulsion and supplementary missions with cargo spacecraft, and you need to support ast

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  • In-orbit test method for low earth orbit long-life manned spacecraft

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Embodiment Construction

[0024] 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, the parts of each structure in the drawings will be described separately. It should be noted that the elements that are not shown in the drawings or described in words are forms known to those of ordinary skill in the art .

[0025] 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...

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Abstract

The invention relates to an in-orbit test method for a low earth orbit long-life manned spacecraft. The in-orbit test method for the low earth orbit long-life manned spacecraft comprises the followingsteps of a, in-orbit test carried out after the spacecraft goes into a light orbit; b, in-orbit test carried out before the spacecraft develops a docking and adding mission; and c, in-orbit test carried out during the autonomous flight period of the spacecraft. The in-orbit test method for the low earth orbit long-life manned spacecraft can make targeted test projects and carry out multiple in-orbit tests for different flight stages and the executions of different missions.

Description

technical field [0001] The invention relates to the field of on-orbit management of manned spacecraft, in particular to an on-orbit test method for low-orbit long-life manned spacecraft. Background technique [0002] Manned spacecraft belongs to the category of manned space vehicles that fly autonomously in orbit for a long time and are attended by people in the short or medium term. After the manned spacecraft enters the orbit and completes the initial state setting of the platform, it is necessary to carry out a special on-orbit test on the platform to evaluate the working state of the platform after it enters the orbit. After the evaluation is completed, it will transfer to the long-tube autonomous flight; Carry out rendezvous and docking missions, astronaut on-orbit resident missions, and propulsion and supplementary missions. Since the execution time of these missions is longer than the time for orbital testing, special on-orbit testing of mission-related functions is r...

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Application Information

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IPC IPC(8): B64G3/00G01D21/02
CPCB64G3/00G01D21/02
Inventor 程伟杨宏梁克张璐南洪涛于世强王静华陈朝基王悦张旭
Owner BEIJING SPACE TECH RES & TEST CENT
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