An optimization designing method of fractionated spacecraft

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

1 Scopus citations

Abstract

This article systematically illustrates the concept of the fractionated spacecraft and analyzes the project evaluation and the optimized designs of fractionated spacecraft system from domestic and foreign scholars, then based on those, they presented a new index that random task cycle costs should be regarded as a comprehensive assessment criterion. Next, through modeling the uncertain cost of module development, launch/deployment and full task cycle of Monte Carlo simulation, it provides random task cycle cost of every configuration scheme. Lastly, it establishes the partitioning criteria and partitioning method system for fractionated spacecraft, with further modules' partitioning road map based on pedigree clustering method. The optimized designs are determined according to classification level combined with the actual situations.

Original languageEnglish
Title of host publicationMechanical Engineering, Industrial Electronics and Information Technology Applications in Industry
Pages162-165
Number of pages4
DOIs
StatePublished - 2013
Event2nd International Conference on Mechanical Engineering, Industrial Electronics and Informatization, MEIEI 2013 - Chongqing, China
Duration: 14 Sep 201315 Sep 2013

Publication series

NameApplied Mechanics and Materials
Volume427-429
ISSN (Print)1660-9336
ISSN (Electronic)1662-7482

Conference

Conference2nd International Conference on Mechanical Engineering, Industrial Electronics and Informatization, MEIEI 2013
Country/TerritoryChina
CityChongqing
Period14/09/1315/09/13

Keywords

  • Cycle Cost
  • Designing Method
  • Fractionated Spacecraft
  • Optimization
  • Pedigree Clustering Method

Fingerprint

Dive into the research topics of 'An optimization designing method of fractionated spacecraft'. Together they form a unique fingerprint.

Cite this