2010Contents

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A-1 Refining Membrane Model via Multi Particle Method combined with Vibration Experiment in Vacuum ChamberPDF
A-2 Location of Guided-Pin in Retraction Mechanisms for Large Deployable Space MembranePDF
A-3 Reduction Method of Characteristic Matrices of 2D_ANCF Beam with Using Component Mode Synthesis Method and Experimental ValidationPDF
A-4 Study on deployment of tether on sounding rocket experimentPDF
A-5 Attitude Determination and Control Operation of IKAROS in Initial On-Orbit PhasePDF
A-7 Oscillation-Free Attitude Control System for Spinning Solar Sail and Its Flight ResultsPDF
A-8 Analysis on Membrane Deployment Dynamics of Solar Sail using Multi-Particle ModelPDF
A-9 Image based shape estimation of the membrane of IKAROSPDF
A-10 Orbit and attitude analysis of separated camera attached to IKAROSPDF
A-12 Parameter Estimation of Solar Radiation Pressure Torque of IKAROSPDF
A-13 Estimation of Solar Radiation Pressure Acceleration for IKAROS Spacecraft in the Initial PhasePDF
A-14 Acceleration Estimation and Improvement of Radiation Pressure Model for IkarosPDF
A-15 The extension of the launch window for the H-IIA interplanetary missionPDF
A-18 Application of Multiobjective Design Exploration to SOLAR-C Orbit DesignPDF
A-19 Advanced Descent Solution and Trajectory Generation Scheme for Precise and Safe Lunar Landing MissionPDF
A-21 THE PRELIMINARY ANALYSIS OF THE PERIODICAL ORBIT AROUNT A SMALL ASTEROID MODELED BY THE TWO-MASS MODELPDF

B-2 Trajectory Correction Maneuver of Hayabusa in Earth Reentry PhasePDF
B-4 EDL analysis for "HAYABUSA" reentry and recovery operationPDF
B-6 SHAPE AND REGOLITH DISTRIBUTION OF RUBBLE-PILE ASTEROIDPDF
B-7 Orbital Evolution of Interplanetary Dust Particles around Earthfs Orbit under Solar Radiation PressurePDF
B-8 Approach for Optimal Multi-Rendezvous Trajectory Design for Active Debris RemovalPDF
B-9 Dust Particle Levitation Near Asteroids and the MoonPDF
B-10 A Design of Quasi-Periodic Relative Orbits Using Singular Value Structure of Orbital State Transition MatrixPDF
B-11 Low-Thrust Multiple Rendezvous Trajectories Using Generating FunctionsPDF
B-12 Design of Loose Formation Flying in the Vicinity of Halo Orbits Based on Initial Set ValuesPDF
B-13 Contorol of Formation Flying in Eccentric Orbits with the J2 perturbationPDF
B-14 Orthogonal Constellation by Two Orbiters under PerturbationPDF
B-15 Formation Flight along a Circular Orbit with Pulse InputPDF
B-16 Hayabusa Orbit Determination before Re-entryPDF
B-17 PLANET-C Orbit Determination in Launch PhasePDF
B-20 A study of the guidance approach for the Small Solar Power Sail Demonstrator (IKAROS)PDF
B-21 Consideration for Future Orbit Plan of IKAROSPDF

C-1 Target Selection and Architecture Design for a Manned Near Earth Object MissionPDF
C-2 Landing Strategy of Asteroid Probe Using Multiple MarkersPDF
C-3 Study on penetration performance on constant penetration velocity using all-purpose material test machine.PDF
C-4 Comet Capture Mission |A case study of a capturing method|PDF
C-5 Study of Flying Robot for Mars Explorer with Rotors MechanismPDF
C-8 Maneuverability Analysis of Screw Drive Rover on Soft TerrainPDF
C-9 Proposal of Terramechanics-based Wheel Dynamics Model on Soft GroundPDF
C-10 AUTONOMOUS PATH PLANNING FOR MULTI-VEHICLE WIDE-BASELINE STEREOPDF
C-11 Cluster Flying Configuration Evaluation in the Case of Fractionated Spacecraft ArchitecturePDF
C-12 On Spacecraft Attitude Maneuver using Impulsive ThrustersPDF
C-13 Prospective 3-Axis Attitude Control for Microsatellite byusing Solar Radiation PressurePDF
C-14 A Study on Disturbance Suppression of Reaction Wheel for MicrosatellitePDF
C-15 Analysis and Control of Attitude Motion for Rapid Regional Scanning Earth ObservationsPDF
C-16 Pumping the inclination on the Jupiter equator for the Jupiter Magnetospheric OrbiterPDF
C-17 Jupiter Trojans Rendezvous Mission DesignPDF
C-18 Trajectory Design between Jovian Moons Guided by Invariant ManifoldsPDF
C-19 A study of the transfer trajectories to Halo orbits using stable manifoldsPDF
C-20 Sensitivity Analysis on the Trajectory Design of the Solar Polar Region Observation Mission (Solar Electric Propulsion Option)PDF
C-21 A Study on Trajectory for Round-trip Exploration to Mars Utilizing Deep Space PortPDF