2003Contents ഍ ഍ 2003Contents

഍ ഍ ഍ A-1 Orientation Control of micro satellites by solar paddle motion and actuation mechanism using elastic hinges   ഍ abstract
഍ A-2 Development of Pico-Satellite Separation System and Launch Results   ഍ abstract
഍ A-3 Mode Effects of TVC Nozzle at Ignition od Solid Rocket Motor   ഍ abstract
഍ A-4 Influence of Liquid Sloshing in MUSES-C on Rocket Upper Stage Separation   ഍ abstract
഍ A-5-1 University of Tokyo's CubeSat Launch Results and Its Dynamics   ഍ abstract
഍ A-5-2 Tokyo Tech's CubeSat "CUTE-I"; Operation Reports and Analyses of Pico-SAtellite Dynamics   ഍ abstract
഍ A-6 'NOZOMI' CONSECUTIVE DOUBLE EARTH SWINGBYS FLIGHT TO MARS-GUIDANCE AND NAVIGATION REPORT   ഍ abstract
഍ A-7 Initial Operation of Microwave Discharge Ion Engines onboard "HAYABUSA" Spacecraft of Asteroid Sample Return Space Mission   ഍ abstract
഍ A-8 MUSES-C LAUNCH AND EARLY OPERATIONS REPORT   ഍ abstract
഍ A-9 HAYABUSA, On-orbit Behavior of Attitude Dynamics and Evaluation of Attitude Control System   ഍ abstract
഍ A-10 Result of Reentry Flight Trajectory of USERS Reentry Module (REM)   ഍ abstract
഍ A-11 Angular Momentum Control of Tumbling Spacecraft by Repetitive Impulse Input   ഍ abstract
഍ A-12 Transporting Control of a Failed Satellite Using a Manipulator   ഍ abstract
഍ A-13 A Satellite-Capture Strategy with Bias Initial Momentum   ഍ abstract
഍ A-14 Contact Dynamics and Impedance Matching for Satellite Capture   ഍ abstract
഍ A-15 Deployment Experiment Using S310 Sounding rocket and Its Dynemics Analysis   ഍ abstract
഍ A-16 Deployment Motion of Spin Type Solar Sail   ഍ abstract
഍ A-17 A Study on the Spin Deployment Dynamics of Solar Sail   ഍ abstract
഍ A-18 FEASIBILITY STUDY OF A SOLAR POWER SATELLITE SYSTEM CONFIGURED BY FORMATION FLYING   ഍ abstract
഍ A-19 Initial Investigation on Deployment and Control of Tether-Controlled Spinning Membrane   ഍ abstract
഍ B-1 Guidance and Control for High Speed Flight Demonstration Phase II  ഍ abstract
഍ B-2 STEERING LAW FOR OPTIMAL AERODYNAMICAL ASCENT PATH AND ITS APPLICATION TO GUIDANCE   ഍ abstract
഍ B-3 Robotics Tschnology for MUSES-C Mission -Navigation and Guidance based on Target Marker-   ഍ abstract
഍ B-4 Study on High Accurate Navigation and Guidance for the Lunar Soft Landing Experimental Vehicle (SELENE-B)   ഍ abstract
഍ B-5 A Study on Attitude Representation of Cat Twist and Its Application for Attitude Control of a Satellite   ഍ abstract
഍ B-6 A Study on the Falling Cat Phenomenon   ഍ abstract
഍ B-7 Attitude Control of Two-Wheel-Satellite Considering Maneuver Path   ഍ abstract
഍ B-8 Robust Stabilization of the Angular Velocity of a Rigid Body Based on Zero Dynamics   ഍ abstract
഍ B-9 Simgularity Avoidance Steering Control Law for Control Momentum Gyro System Based on Manipulability   ഍ abstract
഍ B-10 Attitude Control of a Spacecraft Composed of Two Rigid Bodies Using Internal Motion   ഍ abstract
഍ B-11 Analysis of Hopping Method on the Regolith-like Surface   ഍ abstract
഍ B-12 Terramechanics Based Analysis on Traction Mechanics of an Exploration Rover (Evaluation of Climbing Capability on Lunar Regolith Simulant)   ഍ abstract
഍ B-13 Analysis of the Hop Vector in Hopping Mobility   ഍ abstract
഍ B-14 Principle of Mobile System based on Gravitational Field   ഍ abstract
഍ B-15 STUDY ON THE PLANETARY AIRSHIP PLATFORM   ഍ abstract
഍ B-16 In-Orbit Transportation of SSPS Considering Debris Impacts and Cell Degradation by Radiation   ഍ abstract
഍ B-17 Dynamics of the Radially Accelerated Trajectory   ഍ abstract
഍ B-18 Numarical Analysis of the Attitude Control of a Tethered Space Solar Power Satellite   ഍ abstract
഍ B-19 A study of optimization of the steering control law of flying to L4(L5) by electric propulsion   ഍ abstract
഍ B-20 Launch Opportunities for Venus Exploring Missions   ഍ abstract
഍ C-1 An Application of Non-coherent Doppler data for the orbit determination to a spacecraft   ഍ abstract
഍ C-2 Nozomi Orbit Determination and VLBI Obsevation   ഍ abstract
഍ C-3 HAYABUSA orbit Determination under Low Thrust   ഍ abstract
഍ C-4 A STUDY OF RELATIVE NAVIGATION AND GUIDANCE BASED ON ONLY RANGE INFORMATION   ഍ abstract
഍ C-5 Control of Relative Position and Attitude of Spacecrafts using Magnetic Force   ഍ abstract
഍ C-6 On Relative Position Control between Two Spacecraft   ഍ abstract
഍ C-7 Design and Control of Approach Trajectory by Impulsive Velocity Change   ഍ abstract
഍ C-8 Distributed Information Architecture for Large Formation Flight   ഍ abstract
഍ C-9 On the Influence of the Information Sharing in the Formation Control   ഍ abstract
഍ C-10 Test Model and Ground Experiment of VS-CMG for In-Orbit Servicing   ഍ abstract
഍ C-11 Real-time recognition of flat areas for lunar landing using
഍       the shape-form-shading method / Pentland technique   ഍ abstract
഍ C-12 Study on Three Dimensional Space Robot Motion Simulator
഍       Using Network of Personal Computers   ഍ abstract
഍ C-13 Redesign and the Flight Result of the M-V-5 ING   ഍ abstract
഍ C-14 FLIGHT PERFOMANCE OF THE μ-CONTROLLER FOR THE M-V ROCET  ഍ abstract
഍ C-15 An Experiment on Autonomous Control Technology
഍       of Returning to the Target Point Using a Parafoil   ഍ abstract
഍ C-16 Evaluation of the Dynamic Characteristics of Parafoil by Sled Experiments   ഍ abstract
഍ C-17 The Results of Rocket Recovery Demonstrator Vehicle Suspended from Helicopter   ഍ abstract
഍ C-18 Applocation of Input Shaping Control to Slew Manmeuver Problem of a Flexible Space Structure   ഍ abstract
഍ C-19 Experimental Study of Drum Type Space Tether Reel   ഍ abstract
഍ C-20 Deployment / Retrieval Control of a Tethered Satellite with Safe Kinetic Region   ഍ abstract
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