Works matching IS 18840485 AND DT 2019 AND VI 17 AND IP 4
Results: 21
Numerical Analysis on Reusable Rocket Aerodynamics with Reduced-Yaw-Force Configurations.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 4, p. 439, doi. 10.2322/tastj.17.439
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Development of Open Model-based Collaboration Tool and Application on Nano-satellite Project.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 4, p. 412, doi. 10.2322/tastj.17.412
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Effect of Observation by Angle Only Navigation to Plan Non-Cooperative Approach for ADR.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 4, p. 471, doi. 10.2322/tastj.17.471
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The Study on Performance of MEMS IMU for Launch Vehicle under High Vibration Environment.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 4, p. 421, doi. 10.2322/tastj.17.421
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JAXA Space Education Program for Informal Education: A case study of the "Aerospace School" program.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 4, p. 506, doi. 10.2322/tastj.17.506
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Process Optimization Method for the Simplification of Developing Indoor Positioning Environment.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 4, p. 552, doi. 10.2322/tastj.17.552
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Development of Binary Black Hole Observation Satellite "ORBIS".
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 4, p. 477, doi. 10.2322/tastj.17.477
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Observer-based Disturbance Estimation for a Spacecraft Inertial Pointing Using Magnetic Torquers.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 4, p. 447, doi. 10.2322/tastj.17.447
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Thrust-Performance Maximization of Microwave Rocket Sustained by Resonant Magnetic Field.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 4, p. 531, doi. 10.2322/tastj.17.531
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Effects of Impact Angles on Ballistic Limit of Ultra-High-Molecular-Weight Polyethylene Fiber Fabrics.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 4, p. 432, doi. 10.2322/tastj.17.432
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Flight Control Parameter Design for Mars Airplane Balloon Experiment-1 (MABE-1) Using Evolutionary Computation.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 4, p. 512, doi. 10.2322/tastj.17.512
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Error Analysis for CAMUI Type Hybrid Rocket Regression Simulation.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 4, p. 519, doi. 10.2322/tastj.17.519
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OMOTENASHI Trajectory Analysis and Design: Earth-Moon Transfer Phase.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 4, p. 496, doi. 10.2322/tastj.17.496
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Dynamics Analysis of Weathercock like Passive Sun-oriented Control Using Solar Pressure.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 4, p. 483, doi. 10.2322/tastj.17.483
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One-dimensional Ablation Analysis of Lightweight CFRP Ablators with Coking.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 4, p. 461, doi. 10.2322/tastj.17.461
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Implementation of Bus-Type Architecture with Common Subsystem in Microsatellite ORBIS.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 4, p. 491, doi. 10.2322/tastj.17.491
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Simplified Covariance Estimation and Target Observation Management Method for On-Board Optical Navigation of Deep Space Probe.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 4, p. 538, doi. 10.2322/tastj.17.538
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Measurement of Momentum to Move with Hypervelocity Impacts of Projectile.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 4, p. 427, doi. 10.2322/tastj.17.427
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Analysis of the Orbital Transfer between the Earth-Mars Orbit using Electric Propulsion based on the Direct Collocation Method.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 4, p. 455, doi. 10.2322/tastj.17.455
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Tubular Equivalent Regression Rate in Hybrid Rockets with Complex Geometries.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 4, p. 544, doi. 10.2322/tastj.17.544
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Postural Control for Beam-Riding Flight of a Microwave Rocket Using an External Magnetic Field.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 4, p. 525, doi. 10.2322/tastj.17.525
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