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MIYASAKA Akihiro

Profile Research field Research achievement Educational achievement Social contribution achievement

 

Published Papers  
No.TitleJournalVolNoStart PageEnd PagePublication dateDOIReferee
1Design and Rigidity Estimation of an Ultra-lightweight Solar Array Journal of Evolving Space Activities 39 Apr. 2023 https://doi.org/10.57350/jesa.391Refereed 
2Modeling and Evaluation of Inflatable Tubes for Gravity Compensator of Space Deployable Structures 設計工学(Web) 56 341 352 Jun. 2021  
3Proposal of a New Concept for Lightweight Solar Array Structures with High Rigidity TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 19 144 149 Mar. 2021 https://doi.org/10.2322/tastj.19.1441
4Modeling and Evaluation of Inflatable Tubes for Gravity Compensator of Space Deployable Structures JOURNAL OF JAPAN SOCIETY FOR DESIGN ENGINEERING 56 331 342 2021 https://doi.org/10.14953/jjsde.2020.29091
5Experimental Evaluation of Reducing Cable-strain Energy of Tension-truss Surface with compression members Journal of Spacecraft and Rockets 57 835 843 Jul. 2020  Refereed 
6Surface design method incorporating compression members for cable-mesh reflectors Journal of Spacecraft and Rockets 55 214 222 2018 https://doi.org/10.2514/1.A338751Refereed 
7Progress in and Prospects of On-Board Communication Equipment Technologies for Communications Satellites in Japan IEICE TRANSACTIONS ON COMMUNICATIONS E100B 1633 1643 Sep. 2017 https://doi.org/10.1587/transcom.2016PFI00021Refereed 
8Technology Trends for Communication Satellite Antenna Systems The Journal of the Institute of Electrical Engineers of Japan 137 166 169 Mar. 2017 https://doi.org/10.1541/ieejjournal.137.1661Not refereed 
9Design Method for Large Deployable Antenna to Study on Topology of Cable Network The Proceedings of the Space Engineering Conference 2017.26 2A5 2017 https://doi.org/10.1299/jsmesec.2017.26.2a51Not refereed 
10Fundamental Design method of Antenna surface including compression members The Proceedings of Mechanical Engineering Congress, Japan 2017 G1900101 2017 https://doi.org/10.1299/jsmemecj.2017.g19001011Not refereed 
11Design method of cable network including compression member for large deployable antenna Transactions of the JSME (in Japanese) 082 843 16 00162-16-00162 Nov. 2016 https://doi.org/10.1299/transjsme.16-001621Refereed 
12Preliminary research of design procedure for space deployable structures with surfaces of revolution composed of scissors members The Proceedings of the Space Engineering Conference 2016.25 2A3 2016 https://doi.org/10.1299/jsmesec.2016.25.2a31Not refereed 
13J1910101 Conceptual Study of Lightweight Structures for Concentrator Photovoltaic System The Proceedings of Mechanical Engineering Congress, Japan 2014 _J1910101- _J1910101- 2014 https://doi.org/10.1299/jsmemecj.2014._j1910101-1Not refereed 
14P09 Fundamental Research of Relative Motion in Positioning Mechanism Using Kinematic Couplings The Proceedings of the Space Engineering Conference 2013.22 _P09-1_ _P09-3_ 2013 https://doi.org/10.1299/jsmesec.2013.22._p09-1_1Not refereed 
15Thermal behavior of a weatherproof power supply system with built-in nickel-metal hydride batteries developed for stationary use JOURNAL OF POWER SOURCES 194 1156 1163 Dec. 2009 https://doi.org/10.1016/j.jpowsour.2009.06.0141Refereed 
16An air-breathing single cell small proton exchange membrane fuel cell system with AB5-type metal hydride and an ultra-low voltage input boost converter JOURNAL OF POWER SOURCES 186 37 44 Jan. 2009 https://doi.org/10.1016/j.jpowsour.2008.09.0511Refereed 
17Charge/discharge characteristics of a backup power supply system using nickel metal hydride batteries INTELEC 07 - 29TH INTERNATIONAL TELECOMMUNICATIONS ENERGY CONFERENCE, VOLS 1 AND 2 614 620 2007  Refereed 
18Reduction of Heat Generation from Onboard SSPA by Using Heat Suppression Signal JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 52 610 507 513 Nov. 2005 https://doi.org/10.2322/jjsass.52.5071Refereed 
19Heat Suppressing Technique for Onboard Amplifiers by Hub Station Control The IEICE transactions on communications B J88-B 193 196 Jan. 2005  Refereed 
20Experimental Estimation for Thermal Control of Onboard Battery during Charging at the Launch Site JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 52 602 121 128 Mar. 2004 https://doi.org/10.2322/jjsass.52.1211Refereed 
21Visual analysis in a deployable antenna experiment IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS 40 247 258 Jan. 2004 https://doi.org/10.1109/TAES.2004.12921571Refereed 
22A Deploying Process Analysis Using Sub-Pixel Cross-Correlation Method : An Application for Deploying Experiment of Small-Scaled Model of ETS-VIII Deployable Antenna JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 50 587 496 503 Dec. 2002 https://doi.org/10.2322/jjsass.50.4961Refereed 
23Mathematical modeling for predicting steady state and transient characteristics of Reservoir Embedded Looped Heat Pipe (RELHP) SAE Technical Papers 2001 https://doi.org/10.4271/2001-01-22391Refereed 
24Development of Loop Heat Pipe deployable radiator for use on Engineering Test Satellite VIII (ETS-VIII) SAE Technical Papers 2001 https://doi.org/10.4271/2001-01-23411Refereed 
25Thermal Distortion of a Modular Structure for Use a Large Reflector Transactions of the Japan Society of Mechanical Engineers Series B 66 646-A 136 143 Jun. 2000 https://doi.org/10.1299/kikaia.66.12101Refereed 
26Satellite mesh reflector temperature measured by using fine thermocouples Journal of Thermophysics and Heat Transfer 13 164 165 1999 https://doi.org/10.2514/2.64181Refereed 
27Thermal Design Evaluation of Large Reflector Deployment Mechanism by Using Flight Data. Aeronautical and Space Sciences Japan 44 508 284 290 Aug. 1996 https://doi.org/10.2322/jjsass1969.44.2841Refereed 
28A Thermal Design Verification of Large Reflectors Using Flight Data Aeronautical and space sciences Japan 44 506 190 195 Mar. 1996 https://doi.org/10.2322/jjsass1969.44.1901Refereed 
29Experimental results for capillary looped pipe applied to direct cooling method Journal of Thermophysics and Heat Transfer 96 100 1995 https://doi.org/10.2514/3.6331Refereed 
30Deployment mechanism for a large reflector: Thermal-design verification using flight data Journal of Spacecraft and Rockets 32 890 893 1995 https://doi.org/10.2514/3.267011Refereed 
31Thermal design verification of a large deployable antenna for a communications satellite Journal of Spacecraft and Rockets 29 271 278 1992 https://doi.org/10.2514/3.263451Refereed 
32Thermal Design Evaluation of On-Board Large Deployable Antenna. Aeronautical and Space Sciences Japan 39 453 504 512 Oct. 1991 https://doi.org/10.2322/jjsass1969.39.5041Refereed 
33Heat transport performance of axially grooved heat pipe with multiple heating points. Aeronautical and Space Sciences Japan 37 424 222 227 May. 1989 https://doi.org/10.2322/jjsass1969.37.2221Refereed 

 

MISC  
No.TitleJournalVolNoStart PageEnd PagePublication date
1Surface Potential History and Volume Resistivity of Polyimide Film at Cryogenic Temperature 宇宙航空研究開発機構特別資料: 第14回「宇宙環境シンポジウム」講演論文集 = JAXA Special Publication: Proceedings of the 14th Spacecraft Environment Symposium 17 169 173 Jan. 15, 2018 
2Experimental verification of weight reduction effect for cable network with compression members 宇宙科学技術連合講演会講演集(CD-ROM) 62nd 2018 
3Charging Characteristics of Spacecraft Dielectric Material at Cryogenic Temperature 宇宙航空研究開発機構特別資料: 第13回宇宙環境シンポジウム講演論文集 = JAXA Special Publication: Proceedings of the 13th Spacecraft Environment Symposium 16 145 148 Feb. 15, 2017 
4D04 Design method of cable network including compression member for large deployable antenna 2015 24 "D04 1"-"D04-4" Dec. 21, 2015 
5A Study on a structural characteristic of a cable network structure integrated with compression members for accurate large antenna 58 4p Nov. 12, 2014 
6Characteristics of Pneumatic Gravity Compensation System Applied to Three-dimensional Movement of Deployable Structures 58 4p Nov. 12, 2014 
7J1910103 The study on internal pressure character of a gravity compensation device underpinning deploy able space structures Mechanical Engineering Congress, Japan 2014 "J1910103 1"-"J1910103-3" Sep. 7, 2014 
8B04 A Study on Buckling Analysis of Joint for Flexible Multibody Structures 2013 22 "B04 1"-"B04-4" Dec. 20, 2013 
9B03 Optimum Design of Supporting Structure of Cable-Mesh Antenna Reflector 2013 22 "B03 1"-"B03-5" Dec. 20, 2013 
10B2 The Design of Large Deployable Reflector for ETS-VIII 35 41 2001 
11STRUCTURAL DESIGN COORDINATING THERMAL ESTIMATION FOR LARGE DEPLOYABLE REFLECTOR Proceedings of the conference on computational engineering and science 537 540 May. 28, 1997 
12Estimation of the maximum RF power using the acceptance temperature and the efficiency for phased array feeder Technical report of IEICE. SAT 96 316 15 22 Oct. 18, 1996 
13Heat-Transport Characteristics of Capillary Looped Pipes Transactions of the Japan Society of Mechanical Engineers. Series B. 61 582 665 671 Feb. 25, 1995 

 

Conference Activities & Talks  
No.TitleConferencePublication datePromoterVenue
1Pillow Deformation of Cable-mesh Surface Antenna The 34th International Symposium on Space Technology and Science, Jun. 6, 2023 
2Antenna Structural Concept Composed of Scissors Member Connected with Convex Tapes The 34th International Symposium on Space Technology and Science, Jun. 6, 2023 
3Design of Solar Paddle With Improved Power Generation Using Multiple Reflections The 34th International Symposium on Space Technology and Science Jun. 6, 2023 
4Compensator in Large Deployable Structure for Space Using Mecanum Wheel The 34th International Symposium on Space Technology and Science, Jun. 6, 2023 
5Vibration characteristics of ultra-lightweight with high-rigidity solar array structure 33rd International Symposium on Space Technology and Science Mar. 2, 2022 
6Cable-Mesh Surface Design for Large Antenna Including Mesh Deformation 33rd International Symposium on Space Technology and Science Mar. 2, 2022 
7Scissors-Structure Antenna Design on Initial Deployment Force Generated by Strain Energy 33rd International Symposium on Space Technology and Science Mar. 2, 2022 
8Preliminary Investigations of Pneumatic Gravity Compensation System for Deployable Space Structures 31st International Symposium on Space Technology and Scient Jun. 2017 
9Fundamental Design Method of Antenna Surface Including Compression Members 31st International Symposium on Space Technology and Scient Jun. 2017 
10Preliminary Study of Deployable Structures Assembled with Scissors Members Applied for Parabolic Reflectors 31st International Symposium on Space Technology and Scient Jun. 2017 
11Fundamental Study on Vibration Characteristics of Space Solar Power Systems 31st International Symposium on Space Technology and Scient Jun. 2017 
12Preliminary Design Study on Tension Truss Antenna Surface for Shape Stability 31st International Symposium on Space Technology and Scient Jun. 2017 
13High-Precision Positioning of Flexible deployable Structures Using Kinematic Couplings 46th international conference on environmental systems ICES 2016 Oct. 2015 
14Estimation of thermal distortion of reflector formed by truss structure 30th International Symposium on Space and Technology and Sicence Jul. 2015 
15Pneumatic gravity compansation system applied to three-dimensional movement of deployable structure 30th International Symposium on Space and Technology and Sicence Jul. 2015 
16An 80-kWh-class Telecommunications Backup System with Large-scale Nickel Metal Hydride Batteries Telecommunications: The Infrastructure for the 21st Century (WTC) Sep. 2010 
17Artificial Neural Network for State-of-Charge Estimation of a Ni-MH Battery with a Photovoltaic Power System 216th ECS Meeting Oct. 2009 
18Low-current Charge Properties of Large-scale Nickel Metal Hydride Batteries and Application to Photovoltaic Power Generation 214th meeting of ECS Oct. 2009 
19Charge/discharge characteristics of a backup power supply system using nickel metal hydride batteries Telecommunications energy conference Sep. 2007 
20Integration and Testing of Large Deployable Reflector on ETS-VIII AIAA ICSSC-21 Apr. 2003 
21Performances D’un Reflecteur De La Taille D’un Court De Tennis Pour ETS-VIII 12èmes Journées Internationales de Nice sur les Antennes International Symposium on Antennas Nov. 2002 
22A Tennis-court-sized Reflector for Communication Satellites 2002 Joint Conference on Satellite Communications, JC-Sat 2000 Oct. 2002 
23Ground verification Methods for Surface Accuracy of Large Deployable Antenna Reflector 23rd International Symposium on Space Technology and Science May. 2002 
24Development of Loop Heat Pipe Deployable Radiator for Use on Engineering Test Satellite VIII 31st International Conference on Environmental Systems Proceedings Jul. 2001 
25Mathematical Modeling for Predicting Steady State and Transient Characteristics of Reservoir Embedded Looped Heat Pip 31st International Conference on Environmental Systems Proceedings Jul. 2001 
26Design and Ground Verification of Large Deployable Antenna 42nd AIAA/ASME/AHS/ASC Structural Dynamics & Material Apr. 2001 
27Analysis and Test Methods for Large Deployable Space Structure 42nd AIAA/ASME/AHS/ASC Structural Dynamics & Material Apr. 2001 
28Thermal Balance Testing for A Large Deployable Reflector 29th International Conference on Environmental Systems Proceedings Jan. 1999 
29Development of a 15 m Class Modular Mesh Deployable Antenna 48th International Astronautical Congress Oct. 1997 
30Thermal Distortion of Over 10 Meter Diameter Reflectors Formed by Truss Structure AIAA 32nd Thermophysics Conference Jun. 1997 

 

Research Grants & Projects  
No.Offer organizationSystem nameTitleFund classificationDate
1Japan Society for the Promotion of Science Grants-in-Aid for Scientific Research Solar Array with High Power Density for Space Use  Apr. 2020 - Mar. 2023