纳型卫星研制关键技术
|
摘要
纳型卫星的低成本研制与长期可靠运行、微型化需求与现有器/部件水平,以及受限的资源与高性能有效载荷之间形成了3组矛盾。针对上述问题,文章从多学科优化和总体架构设计、微机电器/部件研制方法及高性能有效载荷空间应用方式3个层次开展研究,介绍了基于多学科优化的纳型卫星平台研制技术、星上高性能微机电器/部件技术,以及适用于纳型卫星平台搭载的有效载荷应用技术。研究成果已在我国多个商业卫星星群,以及探月工程、高分专项等任务中进行了批量化应用。
There are three contradictions between the low cost development and the long-term reliable in orbit operation of nanosatellite,the requirements for miniaturization of nanosatellites and the current devices and components,as well as the limited resources and the high performance payload.The overall design based on multidisciplinary optimization,the principle and development method of device and component,and the high performance in orbit application scheme are analyzed considering the above three problems on nanosatellites.The multidisciplinary optimization based nanosatellite platform construction and high efficiency in orbit operation method,the high performance onboard device and component development and the advanced payload application technology for nanosatellite are introduced.The research productions have been applied in batches on many commercial satellite constellations,lunar exploration project and Gaofen project in China.
There are three contradictions between the low cost development and the long-term reliable in orbit operation of nanosatellite,the requirements for miniaturization of nanosatellites and the current devices and components,as well as the limited resources and the high performance payload.The overall design based on multidisciplinary optimization,the principle and development method of device and component,and the high performance in orbit application scheme are analyzed considering the above three problems on nanosatellites.The multidisciplinary optimization based nanosatellite platform construction and high efficiency in orbit operation method,the high performance onboard device and component development and the advanced payload application technology for nanosatellite are introduced.The research productions have been applied in batches on many commercial satellite constellations,lunar exploration project and Gaofen project in China.
引文
[1]NASA.VanguardTV3[EB/OL].[2018-10-20].2018.http://nssdc.gsfc.nasa.gov/nmc/spacecraftDisplay.do?id=VAGT3
[2]Amateur Satellite Service.AMSAT satellite status[EB/OL].[2018-10-20].2018.http://www.amsat.org/amsat-new/satellites/status.phpS
[3]Yamada K,H Nagano.Development of a heat storage panel for micro/nano-satellites and demonstration in orbit[J].Applied Thermal Engineering,2015,91:894-900
[4]Craig Underwood,Craig Pellegrino,Vaios J Lappas,et al.Using CubeSat/micro-satellite technology to demonstrate the Autonomous Assembly of a Reconfigurable Space Telescope(AAReST)[J].Acta Astronautica,2015,114:112-122
[5]Rievers B,A Milke,D Salden.Cubesat in-situ degradation detector(CIDD)[J].Acta Astronautica,2015,112:69-76
[6]Shinichi Nakasuka,Nobutada Sako,Hironori Sahara,et al.Evolution from education to practical use in University of Tokyo’s nano-satellite activities[J].Acta Astronautica,2010,66(7/8):1099-1105
[7]安君帅,张生玥,肖跃.国内外小卫星的发展现状及前景[C]//第十二届卫星通信学术年会论文集.北京:中国通信学会卫星通信委员会,2016:89-96An Junshuai,Zhang Shengyue,Xiao Yue.Development status and prospect of small satellite[C]//Proceedings of the 12th Annual Conference on Satellite Communications.Beijing:Satellite Communications Committee of China Communications Society,2016:89-96(in Chinese)
[8]Dustin Berkovitz,Edmund Kong,David Miller.System identification of the spheres autonomous rendezvous and docking testbed[C]//Proceedings of AIAA Space2003.Washington D.C.:AIAA,2003:23-25
[9]R Roubache,M Benyettou,A M Si Mohammed,et al.Impact of the orbital eccentricity on the attitude performance before and after the deorbiting phase for Alsat-1[J].Advances in Space Research,2014,53(3):474-489
[10]M L Battaglierel,F Santonil,F Piergentili,et al.Passive magnetic attitude stabilization system of the EduSAT microsatellite[J].Journal of Aerospace Engineering,2010,224(10):1097-1106
[11]Tzu-Pang Tseng,Cheinway Hwang,Shan Kuo Yang.Assessing attitude error of FORMOSAT-3/COSMICsatellites and its impact on orbit determination[J].Advances in Space Research,2012,49(9):1301-1312
[12]李军予,伍保峰,张晓敏.立方体纳卫星的发展及其启示[J].航天器工程,2012,21(3):80-87Li Junyu,Wu Baofeng,Zhang Xiaomin.Development of CubeSat and its enlightenment[J].Spacecraft Engineering,2012,21(3):80-87(in Chinese)
[13]赵炜渝,白保存,金仲和.皮纳卫星应用与特点分析[J].国际太空,2013(8):36-40Zhao Weiyu,Bai Baocun,Jin Zhonghe.Analysis of pico-satellite application and characteristics[J].Space International,2013(8):36-40(in Chinese)
[14]叶钊,李熹微,王超,等.微纳卫星光学载荷技术发展综述[J].航天器工程,2016,25(6):122-130Ye Zhao,Li Xiwei,Wang Chao,et al.Survey of technological development of optical payload for Micronano satellite[J].Spacecraft Engineering,2016,25(6):122-130(in Chinese)
[15]付俊明.协作优化方法在卫星总体多学科设计优化中的应用研究[D].北京:清华大学,2006Fu Junming.Research on applying collaborative optimization to the multidisciplinary design optimization of satellites design[D].Beijing:Tsinghua University,2006(in Chinese)
[16]Shi S,Yuan B,Zhao K,et al.Fault-tolerant attitude determination and control system design of Nanosatellite 2[J].Journal of Aerospace Engineering,2018,31(6):04018087
[17]Zhou Bin,Chen Zhiyong,Zhang Rong.A digital silicon micromachined gyroscope with enhanced temperature stability[C]//Proceedings of 2010International Symposium on Inertial Technology and Navigation.Tianjin:Editorial Board of Journal of Chinese Inertial Technology,2010:192-195
[18]Wu Lingqi,Tian Zheng,Ren Dahai,et al.A miniature resonant and torsional magnetometer based on lorentz force[J].Micromachines,2018,9(12):doi:10.3390/mi9120666
[19]Ren Dahai,Wu Lingqi,Yan Meizhi,et al.Design and analyses of a MEMS based resonant magnetometer[J].Sensors,2009,9(9):6951-6966
[20]Wei Minsong,Xing Fei,You Zheng,et al.An implementation method based on ERS imaging mode for sun sensor with 1kHz update rate and 1″precision level[J].Optics Express,2013,21(26):32524-32533
[21]Zhao Jiahao,Gao Yongfeng.Electrostatic combdrived actuator for MEMS relay/switch[M]//Micro Electro Mechanical Systems.Singapore:Springer Nature Singapore Pte Ltd.,2018:907-927
[22]高永丰.面内式静电驱动MEMS直流开关研究[D].北京:清华大学,2016Gao Yongfeng.Research on the in-plane electrostatic MEMS DC switch[D].Beijing:Tsinghua University,2016(in Chinese)
[23]Liangchen Y,Gaofei Z,Zheng Y.5Vcompatible two-axis PZT driven MEMS scanning mirror with mechanical leverage structure for miniature LiDAR application[J].Sensors,2017,17(3):521
[2]Amateur Satellite Service.AMSAT satellite status[EB/OL].[2018-10-20].2018.http://www.amsat.org/amsat-new/satellites/status.phpS
[3]Yamada K,H Nagano.Development of a heat storage panel for micro/nano-satellites and demonstration in orbit[J].Applied Thermal Engineering,2015,91:894-900
[4]Craig Underwood,Craig Pellegrino,Vaios J Lappas,et al.Using CubeSat/micro-satellite technology to demonstrate the Autonomous Assembly of a Reconfigurable Space Telescope(AAReST)[J].Acta Astronautica,2015,114:112-122
[5]Rievers B,A Milke,D Salden.Cubesat in-situ degradation detector(CIDD)[J].Acta Astronautica,2015,112:69-76
[6]Shinichi Nakasuka,Nobutada Sako,Hironori Sahara,et al.Evolution from education to practical use in University of Tokyo’s nano-satellite activities[J].Acta Astronautica,2010,66(7/8):1099-1105
[7]安君帅,张生玥,肖跃.国内外小卫星的发展现状及前景[C]//第十二届卫星通信学术年会论文集.北京:中国通信学会卫星通信委员会,2016:89-96An Junshuai,Zhang Shengyue,Xiao Yue.Development status and prospect of small satellite[C]//Proceedings of the 12th Annual Conference on Satellite Communications.Beijing:Satellite Communications Committee of China Communications Society,2016:89-96(in Chinese)
[8]Dustin Berkovitz,Edmund Kong,David Miller.System identification of the spheres autonomous rendezvous and docking testbed[C]//Proceedings of AIAA Space2003.Washington D.C.:AIAA,2003:23-25
[9]R Roubache,M Benyettou,A M Si Mohammed,et al.Impact of the orbital eccentricity on the attitude performance before and after the deorbiting phase for Alsat-1[J].Advances in Space Research,2014,53(3):474-489
[10]M L Battaglierel,F Santonil,F Piergentili,et al.Passive magnetic attitude stabilization system of the EduSAT microsatellite[J].Journal of Aerospace Engineering,2010,224(10):1097-1106
[11]Tzu-Pang Tseng,Cheinway Hwang,Shan Kuo Yang.Assessing attitude error of FORMOSAT-3/COSMICsatellites and its impact on orbit determination[J].Advances in Space Research,2012,49(9):1301-1312
[12]李军予,伍保峰,张晓敏.立方体纳卫星的发展及其启示[J].航天器工程,2012,21(3):80-87Li Junyu,Wu Baofeng,Zhang Xiaomin.Development of CubeSat and its enlightenment[J].Spacecraft Engineering,2012,21(3):80-87(in Chinese)
[13]赵炜渝,白保存,金仲和.皮纳卫星应用与特点分析[J].国际太空,2013(8):36-40Zhao Weiyu,Bai Baocun,Jin Zhonghe.Analysis of pico-satellite application and characteristics[J].Space International,2013(8):36-40(in Chinese)
[14]叶钊,李熹微,王超,等.微纳卫星光学载荷技术发展综述[J].航天器工程,2016,25(6):122-130Ye Zhao,Li Xiwei,Wang Chao,et al.Survey of technological development of optical payload for Micronano satellite[J].Spacecraft Engineering,2016,25(6):122-130(in Chinese)
[15]付俊明.协作优化方法在卫星总体多学科设计优化中的应用研究[D].北京:清华大学,2006Fu Junming.Research on applying collaborative optimization to the multidisciplinary design optimization of satellites design[D].Beijing:Tsinghua University,2006(in Chinese)
[16]Shi S,Yuan B,Zhao K,et al.Fault-tolerant attitude determination and control system design of Nanosatellite 2[J].Journal of Aerospace Engineering,2018,31(6):04018087
[17]Zhou Bin,Chen Zhiyong,Zhang Rong.A digital silicon micromachined gyroscope with enhanced temperature stability[C]//Proceedings of 2010International Symposium on Inertial Technology and Navigation.Tianjin:Editorial Board of Journal of Chinese Inertial Technology,2010:192-195
[18]Wu Lingqi,Tian Zheng,Ren Dahai,et al.A miniature resonant and torsional magnetometer based on lorentz force[J].Micromachines,2018,9(12):doi:10.3390/mi9120666
[19]Ren Dahai,Wu Lingqi,Yan Meizhi,et al.Design and analyses of a MEMS based resonant magnetometer[J].Sensors,2009,9(9):6951-6966
[20]Wei Minsong,Xing Fei,You Zheng,et al.An implementation method based on ERS imaging mode for sun sensor with 1kHz update rate and 1″precision level[J].Optics Express,2013,21(26):32524-32533
[21]Zhao Jiahao,Gao Yongfeng.Electrostatic combdrived actuator for MEMS relay/switch[M]//Micro Electro Mechanical Systems.Singapore:Springer Nature Singapore Pte Ltd.,2018:907-927
[22]高永丰.面内式静电驱动MEMS直流开关研究[D].北京:清华大学,2016Gao Yongfeng.Research on the in-plane electrostatic MEMS DC switch[D].Beijing:Tsinghua University,2016(in Chinese)
[23]Liangchen Y,Gaofei Z,Zheng Y.5Vcompatible two-axis PZT driven MEMS scanning mirror with mechanical leverage structure for miniature LiDAR application[J].Sensors,2017,17(3):521