CubeSat结构热控案
摘要
CubeSat以体积小、成本低、研制周期短等优点受到越来越广泛的关注,但CubeSat的高度集成化、模块化设计对结构热控提出了更高的要求,而且宇宙中的辐射也会对立方体卫星造成影响。本文在参考国外高校对CubeSat的结构热控和辐射防护方案基础上,对结构热控与辐射防护方案进行分析与讨论,给出更理想的方案。
CubeSat is more and more popular because of its peculiarity such as smaller size,low costing and short build-time.However,because it is Highly Integrated and modular,we are requested to do better when we are designing automation for satellite thermal control.At the same time,the radiation in the space will also has impact on our CubeSat.This paper aim to analyze,discuss and present a more ideal scheme using genetic algorithm after reading scheme other school offered.
CubeSat is more and more popular because of its peculiarity such as smaller size,low costing and short build-time.However,because it is Highly Integrated and modular,we are requested to do better when we are designing automation for satellite thermal control.At the same time,the radiation in the space will also has impact on our CubeSat.This paper aim to analyze,discuss and present a more ideal scheme using genetic algorithm after reading scheme other school offered.
引文
[1]王忠强.基于碳纤维复合材料的立方体卫星结构热控一体化设计.
[2]TYPES OF RADIATION in Space.
[3]Emanuel Escobar,Marcos Diaz,Juan Cristóbal Zagal,DESIGN AUTOMATION FOR SATELITE PASSIVE THERMAL CONTROL.
[4]Active Thermal Control System for Cube Sat.
[5]Thomsen D L I,Kim W,Cutler J W.Shields-1,A Small Sat Radiation Shielding Technology Demonstration[J].2015.
[6]Zhao T S. Applied Thermal Engineering[J]. Applied Thermal Engineering,1996,89:968-977.
[7]Escobar E,Diaz M,Zagal J C. DESIGN AUTOMATION FOR SATELLITE PASSIVE THERMAL CONTROL[J].4s Symposium,2012.
[8] D. Rockberger.(2009)Thermal and Mechanical Optimisation of the First Israeli Nanosatellite,Proceedings of the49th Israel annual conference on aerospace sciences.
[9]《Thermal Modeling of Nanosat》,Dai Dinh,from San Jose State University.
[10]《Cube Sat Thermal Analysis》Pradeep Shinde,Alvaro Quintero,Ibrahim Tansel,Sabri Tosunoglu.
[11]刘佳.李运泽.常静.盛江.微小卫星热控系统的研究现状及发展趋势[J].航天器环境工程,2011,28(1):77-82.
[12]潘维,赵欣.小卫星全被动热设计及其验证技术.
[13]麻慧涛,钟奇,范含林,文耀普.微型卫星热控制技术研究.
[14]Thermovacuum Tests on TIGRIsat structure Claudio Paris,Maurizio Parisse.
[15]On-Orbit Thermal Design and Validation of 1U Standardized Cube Sat of STEP Cube Lab.
[16]Thermal analysis of TRIO-CINEMA mission.
[17]Design automation for satellite passive thermal control.
[2]TYPES OF RADIATION in Space.
[3]Emanuel Escobar,Marcos Diaz,Juan Cristóbal Zagal,DESIGN AUTOMATION FOR SATELITE PASSIVE THERMAL CONTROL.
[4]Active Thermal Control System for Cube Sat.
[5]Thomsen D L I,Kim W,Cutler J W.Shields-1,A Small Sat Radiation Shielding Technology Demonstration[J].2015.
[6]Zhao T S. Applied Thermal Engineering[J]. Applied Thermal Engineering,1996,89:968-977.
[7]Escobar E,Diaz M,Zagal J C. DESIGN AUTOMATION FOR SATELLITE PASSIVE THERMAL CONTROL[J].4s Symposium,2012.
[8] D. Rockberger.(2009)Thermal and Mechanical Optimisation of the First Israeli Nanosatellite,Proceedings of the49th Israel annual conference on aerospace sciences.
[9]《Thermal Modeling of Nanosat》,Dai Dinh,from San Jose State University.
[10]《Cube Sat Thermal Analysis》Pradeep Shinde,Alvaro Quintero,Ibrahim Tansel,Sabri Tosunoglu.
[11]刘佳.李运泽.常静.盛江.微小卫星热控系统的研究现状及发展趋势[J].航天器环境工程,2011,28(1):77-82.
[12]潘维,赵欣.小卫星全被动热设计及其验证技术.
[13]麻慧涛,钟奇,范含林,文耀普.微型卫星热控制技术研究.
[14]Thermovacuum Tests on TIGRIsat structure Claudio Paris,Maurizio Parisse.
[15]On-Orbit Thermal Design and Validation of 1U Standardized Cube Sat of STEP Cube Lab.
[16]Thermal analysis of TRIO-CINEMA mission.
[17]Design automation for satellite passive thermal control.