Model Based Systems Engineering (MBSE) Applied to Radio Aurora Explorer (RAX) CubeSat Mission Operational Scenarios

被引:0
|
作者
Spangelo, Sara C. [1 ]
Cutler, James [1 ]
Anderson, Louise [2 ]
Fosse, Elyse [2 ]
Cheng, Leo [2 ]
Yntema, Rose [3 ]
Bajaj, Manas [3 ]
Delp, Chris [2 ]
Cole, Bjorn [2 ]
Soremekum, Grant [4 ]
Kaslow, David [5 ]
机构
[1] Univ Michigan, 1320 Beal St, Ann Arbor, MI 48104 USA
[2] CALTECH, Jet Prop Lab, 4800 Oak Grove Dr, Pasadena, CA 91109 USA
[3] InterCAX, Atlanta, GA 30308 USA
[4] Phoenix Integrat, Blacksburg, VA 24060 USA
[5] Anal Graph, Extron, PA 19341 USA
基金
加拿大自然科学与工程研究理事会;
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Small satellites are more highly resource-constrained by mass, power, volume, delivery timelines, and financial cost relative to their larger counterparts. Small satellites are operationally challenging because subsystem functions are coupled and constrained by the limited available commodities (e. g. data, energy, and access times to ground resources). Furthermore, additional operational complexities arise because small satellite components are physically integrated, which may yield thermal or radio frequency interference. In this paper, we extend our initial Model Based Systems Engineering (MBSE) framework developed for a small satellite mission by demonstrating the ability to model different behaviors and scenarios. We integrate several simulation tools to execute SysML-based behavior models, including subsystem functions and internal states of the spacecraft. We demonstrate utility of this approach to drive the system analysis and design process. We demonstrate applicability of the simulation environment to capture realistic satellite operational scenarios, which include energy collection, the data acquisition, and downloading to ground stations. The integrated modeling environment enables users to extract feasibility, performance, and robustness metrics. This enables visualization of both the physical states (e. g. position, attitude) and functional states (e. g. operating points of various subsysterns) of the satellite for representative mission scenarios. The modeling approach presented in this paper offers satellite designers and operators the opportunity to assess the feasibility of vehicle and network parameters, as well as the feasibility of operational schedules. This will enable future missions to benefit from using these models throughout the full design, test, and fly cycle. In particular, vehicle and network parameters and schedules can be verified prior to being implemented, during mission operations, and can also be updated in near real-time with operational performance feedback.
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收藏
页数:18
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