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Based on central composite design method satellite mission design

  • Beihang University

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

In conceptual design phase, the goal of the satellite mission design is to gain a feasible solution. Satellite mission design involves many domains that are coupling with each other. Usually the domain factors are nonlinear and the interactive effects exist. Therefore, it is difficult to find the best solution if only analyzed one domain factors' main effect. Coupling relationship between the domains must be considered. During the satellite design process, the design team should determine which factors have main effects and which factors have interactive effects. According to the response surfaces, the design team can select the best feasible solution. In this paper, a central composite design method was described. The central composite design method is an optimization method based on statistical data analysis. And it is also a response surface design method. In this method, the design factors are divided into two subsets. One subset is used to estimate the linear and interactive effects. The other subset is used to estimate the curve effects. This method uses the minimum tests to gain the variables and variance information. And it can provide main effect, interactive effect in a graphical fashion. An earth observation satellite mission is as an example. The mission objectives include two points. One is to maximize the best observation days of a region, and the other is to minimize the cost. The simulation models are established on orbit prediction, the visible field, data transmission, and satellite cost. 8 design factors are selected and 145 tests are performed. The simulation results show the orbit variables have main effect and interactive effect on best observation days, but have extremely small effect on the cost. The payload aperture diameter has the main effect on the cost. However, the combination of a small aperture diameter and a high orbit altitude leads to the violation of the resolution constraint. The central composite design method is dependent for each domain design model. This method is able to steer the choices of the design team in a graphical fashion.

源语言英语
主期刊名63rd International Astronautical Congress 2012, IAC 2012
9299-9304
页数6
出版状态已出版 - 2012
活动63rd International Astronautical Congress 2012, IAC 2012 - Naples, 意大利
期限: 1 10月 20125 10月 2012

出版系列

姓名Proceedings of the International Astronautical Congress, IAC
11
ISSN(印刷版)0074-1795

会议

会议63rd International Astronautical Congress 2012, IAC 2012
国家/地区意大利
Naples
时期1/10/125/10/12

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