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Japan Society for Aeronautical and Space Sciences | 論文
- Instability Waves Developing from a Point Source near the Attachment Line on a Yawed Circular Cylinder
- Buckling of Circular Cylindrical Shell under Beam-Like Bending (1st Report) Experiment
- Calculation on flat plate cascade with dead water region of Kirchhoff type and with high subsonic free streamline.
- Disturbance Preview Controller and Its Application to a Small UAV
- Analysis of Noise Failure Characteristics for Superluminescent Diode Fiber-Optic Gyroscopes in Space Applications
- Analysis and Control of Attitude Motion for Rapid Regional Scanning Earth Observations
- Effects of Heat Transfer in Divergent Section of Laval Nozzle on Exhaust Velocity and Area Ratio
- Differential Game Guidance Law for Interceptor Missiles with a Time-varying Lateral Acceleration Limit
- Bounded Linear-Quadratic Differential Game Guidance Law for Dual-Thruster Controlled Missiles
- Experimental Study on Estimation of Upper Limit of Ammonium Perchlorate Content in Ammonium Perchlorate/Hydroxyl-Terminated Polybutadiene Composite Propellant
- Determining Novel Periodic Orbits around Equilibrium Points of Asteroids
- Numerical Study of Start Strategy for Ram Accelerator at the Time of Low Injection Pressure
- Numerical Study of Shock-Wave Reflections from a Wedge with Surface Roughness
- Unsteady Aerodynamic Analysis and Wake Simulation of Helicopter Rotors using the Time-Domain Panel Method
- Evaluation of Solar Power Satellite Designed by SPS Feasibility, Committee in Japan : Its Energy Cost and Influences on Earth's Ecology and Economics
- Instability Characteristics of a Free-Free Multi-Stepped Timoshenko Beam with Concentrated Masses Subjected to Follower Force
- Robust Attitude Control and Compensation under Actuator Practical Restrictions
- Optical Measurement of Plasma Oscillations in a Hall Thruster
- Ram Accelerator Operation Analysis in Thermally Choked and Transdetonative Propulsive Modes
- Improvements in Small-scale Helicopter Rotor Modeling for the Real-time Simulation of Hovering Flight