Interaction system and interaction method for process design and assembly execution of spacecraft final assembly

A technology for spacecraft assembly and process design. It is applied in the fields of instrumentation, computing, and electrical digital data processing. It can solve the problems of low work efficiency, inability to exchange information in real time, and poor compatibility of process data transmission, so as to improve efficiency and realize timely transmission. Effect

Active Publication Date: 2019-07-26
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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Problems solved by technology

[0005] The technical problem to be solved by the present invention is to provide an interactive system for process design and assembly execution for spacecraft assembly, which solves the problem of poor process data transfer compatibility in the prior art, and the lack of real-time information interaction in process design and assembly execution links. The problem of low efficiency, so as to ensure the consistency of process data in process design and assembly execution

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  • Interaction system and interaction method for process design and assembly execution of spacecraft final assembly
  • Interaction system and interaction method for process design and assembly execution of spacecraft final assembly

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Embodiment Construction

[0029] The technical solutions of the present invention will be clearly and completely described below in conjunction with the accompanying drawings and specific embodiments. These embodiments are all exemplary and are not intended to limit the protection scope of the present invention.

[0030] figure 1 Implement an interactive system for process design and assembly for spacecraft final assembly. The process design and assembly execution interactive system for spacecraft assembly of the present invention includes a process design subsystem and an assembly execution subsystem; the process design subsystem includes a process design module 101, a process approval module 102, and a process sending module 103; the process design The module 101 provides a unified process design environment for generating original structured process data. The process design module 101 includes a supporting information editing module 108, a process attachment editing module 109, an operation step ed...

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Abstract

The invention discloses a process design and assembling execution interaction system for spacecraft assembling. The system comprises a process design subsystem and an assembling execution subsystem, wherein the process design subsystem comprises a process design module, a process examining and approving module and a process sending module; and the assembling execution subsystem comprises an assembling execution module, a process receiving interface, a state query interface and a process locking interface. The invention furthermore discloses a corresponding interaction method. By converting allbusiness objects in process data into XML texts, the capability of compatibility with different process contents is improved; and through interaction of the interfaces in the process module and the assembling execution module, timely transmission of process data and immediate feedback of a process execution state are realized, so that the spacecraft assembling efficiency is improved.

Description

technical field [0001] The invention belongs to the technical field of spacecraft assembly, and in particular relates to a process design and assembly execution interaction system and an interaction method for spacecraft assembly. Background technique [0002] In traditional spacecraft assembly work, process design and assembly execution are independently completed by Computer Aided Process Planning (CAPP) and Manufacturing Execution System (MES). The process design results in CAPP, that is, the process data are mainly operation steps and process drawings, which are exported to the specific database of the intermediate server at one time, and then read by the MES system for assembly execution. [0003] Since the database in the intermediate server is defined for a specific CAPP system, it is necessary to re-modify the design of the database when the data source changes. For example, in the manufacturing mode based on the 3D model, the CAPP system not only needs to transmit ...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F17/50
Inventor 韩兴龙李曼丽张旭明赵永平李梦张海英徐佳佳邱逸昌周乐袁坤赵璐潘尚洁万毕乐贺文兴
Owner BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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