|Table of Contents|

Key technologies in integrated design platform for orbit divert and attitude control system(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2015年06期
Page:
27-34
Research Field:
研究与设计
Publishing date:

Info

Title:
Key technologies in integrated design platform for orbit divert and attitude control system
Author(s):
HU Haifeng;  LI Xiaojin;  WANG Hongrang;  LI Ping
Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
Keywords:
digitization designorbit divert and attitude control systempropulsion systemkey technology
PACS:
V434-34
DOI:
-
Abstract:
In order to support the digital design for orbit divert and attitude control system, the framework of the integrated design platform for the orbit divert and attitude control system is presented. The five framework structures of resource, service, integration, prototype and application, and their functions are discussed in detail. The four key technologies (collaborative management in design process, data flow and data management in design activity, knowledge database construction and knowledge push application) are investigated. The corresponding solutions for the key technologies are proposed. The collaborative management system in 3D design process, three-V type data flow organization mode, knowledge database management mechanism in three layers are presented in this paper. Both the technological process push and automatic analysis push methods are put forward for knowledge push. The feasibility of the integrated design platform functions and technologies are discussed. It can be regarded as an antecedence investigation for the building of follow-up platform.

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