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Propellantless Close-Range Guidance for Small Satellite Docking Using Simple Electromagnetic Devices 基于简单电磁装置的小卫星无推进剂近距离对接制导
Yuki Yamada, T. Inamori
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引用次数: 0
Verification of Fully Autonomous Flight from Takeoff to Landing of a Low-Speed Model Airplane with Application to a Small Unmanned Supersonic Airplane 低速模型飞机从起飞到着陆的完全自主飞行验证及其在小型无人超音速飞机上的应用
M. Ueba, Tomohiro Kamata, Sakurako Nakajima, Yosuke Maeda
{"title":"Verification of Fully Autonomous Flight from Takeoff to Landing of a Low-Speed Model Airplane with Application to a Small Unmanned Supersonic Airplane","authors":"M. Ueba, Tomohiro Kamata, Sakurako Nakajima, Yosuke Maeda","doi":"10.2322/tastj.19.667","DOIUrl":"https://doi.org/10.2322/tastj.19.667","url":null,"abstract":"","PeriodicalId":120185,"journal":{"name":"TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN","volume":"5 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126093110","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 2
Fundamental Study on Plant-based Regenerative Life-support Systems with Sweetpotato Culture in Space 甘薯空间培养植物再生生命维持系统的基础研究
Yoshiki Kitaya, K. Higashi, T. Shibuya, R. Endo
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引用次数: 1
Point Cloud-Based Spacecraft Self-Localization for Distant Small Body Exploration 基于点云的航天器远距离小体探测自定位
Shuya Kashioka, Genki Ohira, Y. Takao, T. Iyota, Y. Tsuda
{"title":"Point Cloud-Based Spacecraft Self-Localization for Distant Small Body Exploration","authors":"Shuya Kashioka, Genki Ohira, Y. Takao, T. Iyota, Y. Tsuda","doi":"10.2322/tastj.21.19","DOIUrl":"https://doi.org/10.2322/tastj.21.19","url":null,"abstract":"","PeriodicalId":120185,"journal":{"name":"TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN","volume":"31 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114257468","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
A Project Useful for Starry Sky Protection by Collaboration between Night Time Artificial Light Observation from Space and Night Sky Brightness Observation on the Ground 夜间空间人工光观测与地面夜空亮度观测协同保护星空的有益项目
T. Nakajo, Shusaku Yamaura, F. Onoma, Mayuko Shibayama, Takashi Aoyama, Y. Kato, Yasutake Ito, Hideyuki Kato
{"title":"A Project Useful for Starry Sky Protection by Collaboration between Night Time Artificial Light Observation from Space and Night Sky Brightness Observation on the Ground","authors":"T. Nakajo, Shusaku Yamaura, F. Onoma, Mayuko Shibayama, Takashi Aoyama, Y. Kato, Yasutake Ito, Hideyuki Kato","doi":"10.2322/tastj.19.845","DOIUrl":"https://doi.org/10.2322/tastj.19.845","url":null,"abstract":"","PeriodicalId":120185,"journal":{"name":"TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN","volume":"12 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"125611959","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Performance of a Throttleable Solid Propellant Microthruster Using Laser Heating 激光加热可节流固体推进剂微推力器性能研究
Satoshi Ikuta, Daichi Haraguchi, Yasuyuki Yano, Akira Kakami
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引用次数: 1
The Study on Performance of MEMS IMU for Launch Vehicle under High Vibration Environment 运载火箭MEMS IMU在高振动环境下的性能研究
E. Shimane, S. Matsumoto, Takafumi Moriguchi, Yuzo Iwai, Ryohei Uchino
Accuracy of MEMS gyroscope and MEMS accelerometer h as been improving in recent years and JAXA has been studying a navigation grade Inertial Measurement Un it (IMU) using MEMS gyroscope and MEMS acceleromete r for launch vehicles. One of issues for applying MEMS IM U for launch vehicles is to maintain measurement ac curacy under high vibration environment during launch phase. Thu s we developed a trial model of high accuracy MEMS I U and evaluated the measurement accuracy of the MEMS IMU under high vibration environment by random vibratio n test. This paper presents the issues of MEMS IMU for launch ve icl s, the trial model of MEMS IMU, and evaluation results of the MEMS IMU under high vibration environment.
近年来,MEMS陀螺仪和加速度计的精度不断提高,JAXA正在研究一种用于运载火箭的导航级惯性测量单元(IMU),该单元采用MEMS陀螺仪和加速度计。在运载火箭上应用MEMS IM U的问题之一是在发射阶段高振动环境下保持测量精度。因此,我们开发了高精度MEMS IMU的试验模型,并通过随机振动测试评估了MEMS IMU在高振动环境下的测量精度。本文介绍了用于发射的MEMS IMU的相关问题、MEMS IMU的试验模型以及MEMS IMU在高振动环境下的评估结果。
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引用次数: 4
Ablative Performance of High Density Carbon Phenolic after Cold Soak Exposure 高密度碳酚醛冷浸后的烧蚀性能
K. Hirai, Akiko Nakazato, H. Yano, Kenichi Kawazone, J. Koyanagi, Kazuhiko Yamada
Ablative performance of High-density carbon phenolic (HD-CFRP) is investigated by exposing to an extremely cold temperature of -160 degree Celsius, followed by rapid heating conditions ranging from 5.5 to 12.1 MW/m 2 of JAXA/ISAS arc jet tests to identify the thermal integrity of the material as a future re-entry capsule heat shield material with demanding system requirements, In this paper, we introduce our activities and the outcomes by the investigation.
研究了高密度碳酚醛(HD-CFRP)的烧蚀性能,通过暴露在-160摄氏度的极冷温度下,然后在5.5至12.1 MW/ m2的快速加热条件下进行JAXA/ISAS电弧喷射试验,以确定该材料的热完整性,作为要求苛刻的系统要求的未来返回舱隔热材料。
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引用次数: 2
Development and Attitude Disturbance Estimation of Separation Mechanism for Nano Moon Lander OMOTENASHI 纳米月球着陆器分离机构研制及姿态扰动估计
J. Kikuchi, T. Hashimoto, M. Otsuki, Naoki Morishita, Wataru Torii, Kakeru Tokunaga, Takahiro Kuhara, Kazuyuki Nakamura
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引用次数: 1
JAXA Space Education Program for Informal Education: A Case Study of the “Aerospace School” Program 日本宇宙航空研究开发机构非正式教育空间教育计划:“航天学校”计划的案例研究
Keiko Miyata
JAXA offers a program called “Aerospace School” to high school students as a form of informal education. Participants are divided into teams and work together to come up with a theme for their mission at various JAXA facilities. They also allocate roles and responsibilities among themselves. The goal is not only to provide Science, Technology, Engineering and Mathematics (STEM) knowledge, but also to build their confidence. We hope this experience will help young adults think about their future career paths, and we strive to actively help them realize their potential. This paper presents the methods, specific examples of, and changes to the Aerospace School program that occurred between 2014 and 2017.
JAXA为高中生提供了一个名为“航空学校”的项目,作为一种非正式教育形式。参与者被分成小组,在JAXA的各个设施中一起工作,为他们的任务提出主题。他们还在彼此之间分配角色和责任。目标不仅是提供科学、技术、工程和数学(STEM)知识,而且要建立他们的信心。我们希望这段经历能帮助年轻人思考他们未来的职业道路,我们努力积极帮助他们实现自己的潜力。本文介绍了2014年至2017年间航空航天学院项目的方法、具体例子和变化。
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引用次数: 0
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