宇宙システム工学

研究成果

年別の研究成果 1982 2004 2005 2006 2008 2009 2010 2011 2013 2014 2015 2016 2017 2020 2021 2022 2024 2025

• 193 会議への寄与
• 166 学術誌
• 43 学会誌
• 41 会議記事
• 18 その他
  • 6 章
  • 3 コメント/討論
  • 3 編集
  • 3 総説
  • 2 章 (査読審査付き)
  • 1 前書き/後書き

年別の研究成果

年別の研究成果

検索結果

• 2024

  Adaptive relative orbit control considering laser ablation uncertainty

  Isobe, S., Yoshimura, Y., Hanada, T., Itaya, Y. & Fukushima, T., 2024, (印刷中) In: Journal of Space Safety Engineering.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Control Law 100%
  • Orbit Control 100%
  • Atmospheric Drag 100%
  • Debris Removal 66%
  • Computer Simulation 33%

• Establishment of debris index evaluation criteria and comparison of index effects

  Harada, R., Kawamoto, S. & Hanada, T., 9月 2024, In: Acta Astronautica. 222, p. 586-595 10 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Low Earth Orbit 100%
  • Nearby Object 100%
  • Environmental Impact 50%
  1 被引用数 (Scopus)

• Evaluation of the effectiveness of the 5-year rule — impact on the orbital environment at each altitude by reducing the post-mission disposal lifetime

  Kawamoto, S., Harada, R., Kitagawa, Y. & Hanada, T., 6月 2024, In: Acta Astronautica. 219, p. 653-661 9 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Collision Rate 100%
  • Term Impact 100%
  2 被引用数 (Scopus)

• Formation keeping control for deorbiting an uncooperative satellite by laser ablation

  Isobe, S., Yoshimura, Y., Hanada, T., Itaya, Y. & Fukushima, T., 8月 15 2024, In: Advances in Space Research. 74, 4, p. 1916-1931 16 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Control Law 100%
  • Debris Removal 25%
  • Target Object 25%
  • Relative Position 25%
  • Laser System 25%
  1 被引用数 (Scopus)

• How are multiple satellites seen from the ground? Relative apparent motion and formation stabilization

  Nakajima, K., Yoshimura, Y., Chen, H. & Hanada, T., 3月 2024, In: Astrodynamics. 8, 1, p. 121-134 14 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Apparent Motion 100%
  • Linear Function 100%
  1 被引用数 (Scopus)

• Improved contactless attitude control law of uncooperative spacecraft by laser ablation

  Hayashibara, A., Yoshimura, Y., Hanada, T., Itaya, Y., Fujihara, T. & Fukushima, T., 9月 2024, In: Acta Astronautica. 222, p. 556-562 7 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Feedback Control 100%
  • Environmental Disturbance 100%

• Integrated attitude—orbit control of solar sail with single-axis gimbal mechanism

  Chujo, T., Watanabe, K. & Takao, Y., 12月 2024, In: Astrodynamics. 8, 4, p. 483-506 24 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  Open Access

  • Orbit Control 100%
  • Solar Radiation Pressure 66%
  • Solar Radiation 50%
  • Modeling Error 33%
  • Attitude Control 33%
  1 被引用数 (Scopus)

• Origin identification of sub-millimeter-sized debris from in-situ debris measurements

  Tanahashi, M., Chen, H., Yoshimura, Y. & Hanada, T., 2月 2024, In: Acta Astronautica. 215, p. 449-454 6 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Measurement 100%
  • Orbits 100%
  • Situ Measurement 100%
  • Orbital Parameter 100%
  • In Situ 100%
  2 被引用数 (Scopus)

• Sensitivity analysis for knowledge discovery in scramjet intake design optimization using deep-learning flowfield prediction

  Fujio, C. & Ogawa, H., 7月 2024, In: Aerospace Science and Technology. 150, 109183.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Computer Simulation 100%
  • Design Optimization 100%
  • Computational Cost 100%
  • Deep Learning 100%
  • Tasks 50%
  5 被引用数 (Scopus)

• Stable Orbiting Around Small Moons Using J₂-Perturbed Elliptic Restricted Problem

  Chen, H., Hou, X. & Bando, M., 7月 2024, In: Journal of Guidance, Control, and Dynamics. 47, 7, p. 1327-1340 14 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  Open Access

  • Martian Satellites 100%
  • Three Body Problem 66%
  • Earth's Gravity Field 33%
  • Orbit Maintenance 33%
  • Retrograde Orbit 33%
  1 被引用数 (Scopus)
• 2023

  Capacity of Sun-driven lunar swingby sequences and their application in asteroid retrieval

  Chen, H., 9月 2023, In: Astrodynamics. 7, 3, p. 315-334 20 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Utilization 100%
  • Sun 100%
  • Asteroid 60%
  • Natural Satellites 60%
  • Gravitation 40%
  6 被引用数 (Scopus)

• Fast and reliable prediction of scramjet flowfields via Gaussian process latent variable model and deep learning

  Fujio, C., Akiyama, K. & Ogawa, H., 4月 2023, In: Physics of Fluids. 35, 4, 046120.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  Open Access

  • Gaussian Process 100%
  • Latent Variable Model 100%
  • Deep Learning 100%
  • Models 25%
  • Research Worker 12%
  19 被引用数 (Scopus)

• Fast Prediction of Two-Dimensional Flowfields with Fuel Injection into Supersonic Crossflow via Deep Learning

  Akiyama, K. & Ogawa, H., 2023, In: Transactions of the Japan Society for Aeronautical and Space Sciences. 66, 5, p. 164-173 10 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  Open Access

  • Deep Learning 100%
  • Prediction 100%
  • Two Dimensional 100%
  • Fuel Injection 100%
  • Design 50%
  1 被引用数 (Scopus)

• Sample return system of OKEANOS—The solar power sail for Jupiter Trojan exploration

  Takao, Y., Mori, O., Matsumoto, J., Chujo, T., Kikuchi, S., Kebukawa, Y., Ito, M., Okada, T., Aoki, J., Yamada, K., Sawada, T., Kawasaki, S., Kashioka, S., Oki, Y., Saiki, T. & Kawaguchi, J., 12月 2023, In: Acta Astronautica. 213, p. 121-137 17 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Sample 100%
  • Solar System 100%
  • Solar Energy 100%
  • Sail 100%
  • Jupiter Trojans 100%
  5 被引用数 (Scopus)

• The impact assessment of accidental explosions of large constellations on low earth orbit environment

  Harada, R., Kawamoto, S., Nagaoka, N. & Hanada, T., 6月 2023, In: Journal of Space Safety Engineering. 10, 2, p. 256-263 8 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Environment 100%
  • Low Earth Orbit 100%
  • Impact Assessment 100%
  • Explosion 100%
  • Constellation 100%
  1 被引用数 (Scopus)
• 2022

  Assessing Collision Probability in Low-Thrust Deorbit

  Fukii, S., Sakai, D., Yoshimura, Y., Matsushita, Y., Hanada, T., Itaya, Y. & Fukushima, T., 3月 2022, In: Journal of Space Safety Engineering. 9, 1, p. 47-55 9 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  Open Access

  • Trajectories 100%
  • Supports 50%
  • Environment 50%
  • Parametric Study 50%
  • Mission Success 50%
  3 被引用数 (Scopus)

• Considerations on the lists of the top 50 debris removal targets

  Kawamoto, S., Nagaoka, N., Kitagawa, Y., Harada, R. & Hanada, T., 9月 2022, In: Journal of Space Safety Engineering. 9, 3, p. 455-463 9 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Evolutionary Model 100%
  • Fragmentation 50%
  • Teams 50%
  • Remediation 50%
  • Costs 50%
  5 被引用数 (Scopus)

• Contactless attitude control of an uncooperative satellite by laser ablation

  Sakai, D., Yoshimura, Y., Hanada, T., Itaya, Y. & Fukushima, T., 7月 2022, In: Acta Astronautica. 196, p. 275-281 7 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  Open Access

  • Laser 100%
  • Attitude Control 80%
  • Controllers 60%
  • Normal Vector 40%
  • Simulation 20%
  10 被引用数 (Scopus)

• Deep-learning prediction and uncertainty quantification for scramjet intake flowfields

  Fujio, C. & Ogawa, H., 11月 2022, In: Aerospace Science and Technology. 130, 107931.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  Open Access

  • Prediction 100%
  • Supersonic Combustion 60%
  • Deep Learning 60%
  • Uncertainty Quantification 60%
  • Boundary Layer Separation 40%
  25 被引用数 (Scopus)

• Design optimization and off-design performance analysis of axisymmetric scramjet intakes for ascent flight

  Brahmachary, S., Fujio, C., Aksay, M. & Ogawa, H., 3月 1 2022, In: Physics of Fluids. 34, 3, 036109.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Design 100%
  • Axisymmetric 100%
  • Compression Efficiency 100%
  • High Speed 50%
  • Algorithm 50%
  18 被引用数 (Scopus)

• Improved modeling for design optimization of cusped field thrusters with support of kinetic analysis

  Yeo, S. H., Ogawa, H., Kahnfeld, D., Lewerentz, L. & Schneider, R., 6月 2022, In: Acta Astronautica. 195, p. 465-480 16 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  Open Access

  • Thruster 100%
  • Simulation 50%
  • Fields 50%
  • Performance 50%
  • Design Point 50%
  4 被引用数 (Scopus)

• Mothership-Cubesat Radioscience for Phobos Geodesy and Autonomous Navigation

  Chen, H., Rambaux, N., Lainey, V. & Hestroffer, D., 4月 1 2022, In: Remote Sensing. 14, 7, 1619.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  Open Access

  • Accuracy 100%
  • Geodesy 100%
  • Phobos 100%
  • Investigation 66%
  • Gravitation 66%
  2 被引用数 (Scopus)

• Multi-Objective Design Optimization of Cusped Field Thruster via Surrogate-Assisted Evolutionary Algorithms

  Yeo, S. H. & Ogawa, H., 11月 2022, In: Journal of Propulsion and Power. 38, 6, p. 973-988 16 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Thruster 100%
  • Performance 80%
  • Fields 60%
  • Anode 40%
  • Algorithm 40%
  3 被引用数 (Scopus)

• Nozzle design optimization for supersonic wind tunnel by using surrogate-assisted evolutionary algorithms

  Matsunaga, M., Fujio, C., Ogawa, H., Higa, Y. & Handa, T., 11月 2022, In: Aerospace Science and Technology. 130, 107879.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  Open Access

  • Nozzle 100%
  • Optimization 66%
  • Design 50%
  • Wind Tunnels 50%
  • Boundary Layer 50%
  10 被引用数 (Scopus)

• Physical insights into multi-point global optimum design of scramjet intakes for ascent flight

  Fujio, C. & Ogawa, H., 5月 2022, In: Acta Astronautica. 194, p. 59-75 17 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Global Optimum 100%
  • Compression Efficiency 100%
  • Design 75%
  • Optimum Design 75%
  • Performance 25%
  18 被引用数 (Scopus)

• Space solar power satellite for the Moon and Mars mission

  Baraskar, A., Yoshimura, Y., Nagasaki, S. & Hanada, T., 3月 2022, In: Journal of Space Safety Engineering. 9, 1, p. 96-105 10 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  Open Access

  • Solar Power Satellites 100%
  • Natural Satellites 100%
  • Power Generation 75%
  • Satellites 75%
  • Solar Panel 75%
  26 被引用数 (Scopus)
• 2021

  Fast estimation of internal flowfields in scramjet intakes via reduced-order modeling and machine learning

  Brahmachary, S., Bhagyarajan, A. & Ogawa, H., 10月 1 2021, In: Physics of Fluids. 33, 10, 106110.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Estimation 100%
  • Complex Fluid 100%
  • Scramjets 100%
  • Internals 66%
  • Optimisation Problem 66%
  27 被引用数 (Scopus)

• Heat Loss Analysis of Flow Boiling Experiments Onboard International Space Station with Unclear Thermal Environmental Conditions (1st Report: Subcooled Liquid Flow Conditions at Test Section Inlet)

  Inoue, K., Ohta, H., Toyoshima, Y., Asano, H., Kawanami, O., Imai, R., Suzuki, K., Shinmoto, Y. & Matsumoto, S., 4月 2021, In: Microgravity Science and Technology. 33, 2, 28.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Flow Boiling 100%
  • Heat Losses 87%
  • International Space Station 62%
  • Models 50%
  • Experiments 50%
  17 被引用数 (Scopus)

• Heat Loss Analysis of Flow Boiling Experiments Onboard International Space Station with Unclear Thermal Environmental Conditions (2nd Report: Liquid-vapor Two-phase Flow Conditions at Test Section Inlet)

  Inoue, K., Ohta, H., Asano, H., Kawanami, O., Imai, R., Suzuki, K., Shinmoto, Y., Kurimoto, T. & Matsumoto, S., 10月 2021, In: Microgravity Science and Technology. 33, 5, 57.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Flow Boiling 100%
  • Heat Losses 78%
  • Models 50%
  • Model 50%
  • Experiments 42%
  14 被引用数 (Scopus)

• Multi-fidelity approach for global trajectory optimization using GPU-based highly parallel architecture

  Ueda, S. & Ogawa, H., 9月 2021, In: Aerospace Science and Technology. 116, 106829.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Trajectories 100%
  • Optimization 33%
  • Graphics Processing Unit 33%
  • Design Space 22%
  • Central Processing Unit 22%
  8 被引用数 (Scopus)

• Multipoint design optimization of Busemann-based intakes for scramjet-powered ascent flight

  Brahmachary, S. & Ogawa, H., 2021, In: Journal of Propulsion and Power. 37, 6, p. 850-867 18 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Compression Efficiency 100%
  • Optimization 66%
  • Design Condition 66%
  • Static Pressure 66%
  • Design Optimization 66%
  18 被引用数 (Scopus)

• Numerical investigation of axisymmetric intake flowfield and performance for scramjet-powered ascent flight

  Fujio, C., Brahmachary, S. & Ogawa, H., 4月 2021, In: Aerospace Science and Technology. 111, 106531.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Performance 100%
  • Axisymmetric 66%
  • Trajectories 66%
  • Dynamic Pressure 66%
  • Pressure Drag 66%
  17 被引用数 (Scopus)

• Numerical investigation of combustion characteristics of upstream crescent cavities in a scramjet combustor

  Roos, T., Pudsey, A. & Ogawa, H., 10月 2021, In: Acta Astronautica. 187, p. 43-60 18 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

• Physical insight into axisymmetric scramjet intake design via multi-objective design optimization using surrogate-assisted evolutionary algorithms

  Fujio, C. & Ogawa, H., 6月 2021, In: Aerospace Science and Technology. 113, 106676.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Compression Flow 100%
  28 被引用数 (Scopus)

• Role of solution reconstruction in hypersonic viscous computations using a sharp interface immersed boundary method

  Brahmachary, S., Natarajan, G., Kulkarni, V., Sahoo, N., Ashok, V. & Kumar, V., 4月 2021, In: Physical Review E. 103, 4, 043302.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Heat Flux 100%
  • Immersed Boundary Method 50%
  • Solution Reconstruction 33%
  • Volume 33%
  • Calculation 33%
  11 被引用数 (Scopus)

• The collision avoidance strategy for geostationary satellites considering orbit maintenance

  Sato, K., Yoshimura, Y., Hanada, T., Izumiyama, T. & Shinohara, R., 12月 2021, In: Journal of Space Safety Engineering. 8, 4, p. 331-338 8 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  Open Access

  • Collision Avoidance 100%
  • Orbit Maintenance 100%
  • Thruster 60%
  • Satellites 40%
  • Constraints 40%
  9 被引用数 (Scopus)

• スクラムジェット上昇飛行に向けた流線追跡法によるインテーク設計に関する数値的研究

  寄稿の翻訳タイトル: スクラムジェット上昇飛行に向けた流線追跡法によるインテーク設計に関する数値的研究Chihiro, F. & Hideaki, O., 2月 2021, In: JAXA Special Publication. JAXA-SP-(Web), 20-008, p. 27-36 10 p.

  研究成果: ジャーナルへの寄稿 › 学術誌
• 2020

  Impact on collision probability by post mission disposal and active debris removal

  Kawamoto, S., Nagaoka, N., Sato, T. & Hanada, T., 9月 2020, In: Journal of Space Safety Engineering. 7, 3, p. 178-191 14 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Collision Probability 100%
  • Debris 71%
  • Disposal 71%
  • Altitude 42%
  • Debris Removal 42%
  19 被引用数 (Scopus)

• Light curve approximation using an attitude model of solar sail spacecraft

  Yoshimura, Y., Matsushita, Y., Arakawa, R. & Hanada, T., 2020, In: Journal of Guidance, Control, and Dynamics. 43, 10, p. 1960-1966 7 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  Open Access

  • Bidirectional Reflectance Distribution Function 100%
  • Light Curve 100%
  • Models 66%
  • Solar Radiation Pressure 66%
  • Spacecraft 66%
  3 被引用数 (Scopus)

• Multiobjective optimization and particle-in-cell simulation of cusped field thrusters for microsatellite platforms

  Yeo, S. H., Ogawa, H., Matthias, P., Kahnfeld, D. & Schneider, R., 2020, In: Journal of Spacecraft and Rockets. 57, 3, p. 603-611 9 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Thruster 100%
  • Particle 100%
  • Simulation 66%
  • Fields 66%
  • Design Optimization 66%
  6 被引用数 (Scopus)

• Multi-point design optimization of a high-performance intake for scramjet-powered ascent flight

  Brahmachary, S., Fujio, C. & Ogawa, H., 12月 2020, In: Aerospace Science and Technology. 107, 106362.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Compression Efficiency 100%
  • Performance 66%
  • Characteristics 66%
  • Flow Condition 66%
  • Design Condition 66%
  27 被引用数 (Scopus)

• Numerical investigation of fuel mixing with upstream crescent cavities in a scramjet combustor

  Roos, T., Pudsey, A., Bricalli, M. & Ogawa, H., 12月 2020, In: Acta Astronautica. 177, p. 611-626 16 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Cavity 100%
  • Mechanisms 26%
  • Hybrid 26%
  • Fuel 20%
  • Mixing 20%
  14 被引用数 (Scopus)

• Numerical investigation of upstream cavity enhanced fuel mixing in scramjet combustors

  Roos, T., Pudsey, A., Bricalli, M. & Ogawa, H., 4月 2020, In: Acta Astronautica. 169, p. 50-65 16 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Cavity 100%
  • Combustor 25%
  • Combustion Chamber 25%
  • Mixing 25%
  • Injector 18%
  39 被引用数 (Scopus)

• 太陽活動による大気密度の変化を考慮した小型衛星のデオービットに関する考察

  片山雅之, 外本伸治, 麻生茂 & 平山寛, 2020, In: 航空宇宙技術. 19, 0, p. 47-55 9 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Model 100%
  • Atmospheric Density 100%
  • Universities 66%
  • Aerodynamic Drag 66%
  • Solar Activity 66%
• 2019

  Digital Currency Design for Sustainable Active Debris Removal in Space

  Saito, K., Hatta, S. & Hanada, T., 2月 2019, In: IEEE Transactions on Computational Social Systems. 6, 1, p. 127-134 8 p., 8624313.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  Open Access

  • Debris 100%
  • Debris Removal 100%
  • Currencies 80%
  • Digital Currency 80%
  • Cost 60%
  8 被引用数 (Scopus)

• Estimation of orbital parameters of broken-up objects from in-situ debris measurements

  Kodama, Y., Furumoto, M., Yoshimura, Y., Fujita, K. & Hanada, T., 1月 1 2019, In: Advances in Space Research. 63, 1, p. 394-403 10 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Debris 100%
  • Investigation 60%
  • Estimate 60%
  • Estimates 60%
  • Orbital Parameter 60%
  5 被引用数 (Scopus)

• Particle-in-cell simulation of an optimized high-efficiency multistage plasma thruster

  Matthias, P., Kahnfeld, D., Schneider, R., Yeo, S. H. & Ogawa, H., 10月 1 2019, In: Contributions to Plasma Physics. 59, 9, e201900028.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Thruster 100%
  • Models 66%
  • Simulation 66%
  • Design Optimization 66%
  • Model 66%
  9 被引用数 (Scopus)
• 2018

  An environmental estimation model for in-situ measurements of small space debris

  Furumoto, M. & Hanada, T., 8月 1 2018, In: Advances in Space Research. 62, 3, p. 533-541 9 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Debris 100%
  • Model 85%
  • Models 85%
  • Estimation 71%
  • in Situ Measurement 57%
  5 被引用数 (Scopus)

• Consideration of three-dimensional attitude and position control for a free-floating rigid body using three thrusters

  Matsuno, T., Yoshimura, Y. & Hokamoto, S., 2018, In: International Journal of Aerospace Engineering. 2018, 2825681.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  Open Access

  • State Variable 100%
  • Thruster 100%
  • Lower Class 100%
  • Planning 66%
  • Target Value 66%

• Precise time estimation of on-orbit satellite fragmentations

  Itaya, Y., Fujita, K. & Hanada, T., 11月 2018, In: Acta Astronautica. 152, p. 415-425 11 p.

  研究成果: ジャーナルへの寄稿 › 学術誌 › 査読

  • Hybrid Method 100%
  • Orbits 66%
  • Constraint Equation 66%
  • Orbital Plane 66%
  • Estimates 66%
  3 被引用数 (Scopus)