2001Contents

A-1 Possible Mass Launched to Ulysses-type Solar Polar Orbit by H-UA   abstract
A-2 Retrograde Satellite for Monitoring Geosynchronous Debris
       -Orbit Determination Error Analysis   abstract
A-3 A Study of Optimum Outgoing Trajectories from the L2 Point   abstract
A-4 Conceptual Analysis of an Europa Exploration
       :A Design of Interplanetary Orbits and Feasibility of Aerobraking in Jovian Atmosphere   abstract
A-5 Trajectory Plan and Earth Swingby Operation ofNOZOMI   abstract
A-6 Possibility of Venus Balloons   abstract
A-7 LUNAR-A2003 Launch Orbit Plan Hiroshi   abstract
A-8 Design and Control of Hyaround Trajectory by Impulsive Velocity Change
       Part U: Extension to Three-Dimensional Trajectory   abstract
A-9 MUSES-C Trajectory Design (1998SF36 Target)   abstract
A-10 ISAS VENUS CLIMATE ORBITER MISSION DESIGN   abstract
A-11 ON THE CHATACTERITICS OF THE EDVEGA SCHEME
       WITH APPLICATION TO SOLARSAIL MISSIONS   abstract
A-12 Collision Avoidance Maneuver and Contamination Reduction Maneuver
       in case of The Satellite Separation which used Side-Jet at the M-V rocket   abstract
A-13 Realization of Pure Spin Motion of Spacecraft by Two Wheels   abstract
A-14 Experiment of Antenna Pointing Control for Vehicle-Mounted
       Satellite Communications System   abstract
A-15 APPLICATION OF COEFFICIENT DIAGRAM METHOD
       TO MIMO DESIGN IN AEROSPACE   abstract
A-16 Gain-scheduling control for extending space structures   abstract
A-17 Attitude Control Of A Large Space Structure Having A Movable Crane   abstract
A-18 Acceleration-Level Control of a Space Robot with a Redundant Manipulator   abstract
A-19 A Design of Continuous-Time Adaptive Control Systems for Space Robot
       Manipulations Using Transpose of Generalized Jocobian Matrix   abstract
A-20 Nonholonomic Path Planning of Free Joint Space Manipulator driven by a Reaction Wheel   abstract
A-21 Dynamical Analysis of Redundant Flexible Space Manipulator with Deployable Links   abstract
B-1 GPS-IN-THE-LOOP GNC SYSTEM AND VERTWAL LANDING DYNAMICS
       OF REUSABLE VEHICLE TEST (RVT)   abstract
B-2 An Analysis of Nonlinear Dynamics for the ALFLEX Plane
      - Development of 3D Simulation Software -   abstract
B-3 Optimal Ascent Orbit for Lifting Vehicle with Air Breathing Engine   abstract
B-4 Examination of Reusable Spacecraft Control Using a Parafoil   abstract
B-5 Attitude Synchronization for Tumbling Satellite Motion by Adaptive Sliding Mode Control   abstract
B-6 FlightData Analysis of ETS-VU Space Robotic Experiments   abstract
B-7 Preliminary Study of Satellite Capturing Guidance for Hyper-OSV (Orbital Servicing Vehicle)   abstract
B-8 Feasibility Study of a Formation Flight Control Scheme using Superconductive Magnet   abstract
B-9 A Study on the Navigation and the Control for Formation Right   abstract
B-10 Fuel Saving Control of Tethered Satellite Cluster Systems   abstract
B-11 Error Estimation of Low-Earth-Orbit Determination by Two-Site Optical tracking   abstract
B-12 A Study of Optical Navigation and Guidance   abstract
B-13 OPTICAL AND RADIOMETRIC HYBIRD NAVIGATION FOR MUSES-C   abstract
B-14 Application of VLBI for the orbit determination of the spacecraft   abstract
B-15 A Terrain Recognition Method Using Multiple Images for Soft Landing of Spacecraft   abstract
B-16 Problems in the Orbit Determination Process of the M -V Launch Vehicle Radio Guidance System   abstract
B-17 Orbit Determination Analysis for Nozomi
       considering small V caused by attitude maneuver U   abstract
B-18 Nozomi Orbit Determination in Conjunction Phase   abstract
B-19 A Method to Estimate Absolute Position and Orientation
       of Lunar Rover by using Sun Sensor and Earth Sensor   abstract
B-20 Orbit Determination for Low-thrust interplanetary mission   abstract
B-21 Accuracy of orbit determination for MUSES-C spacecraft   abstract
C-1 Evaluation of internal disturbances caused by rotary instruments
       located on the satellite and disturbances detection experiment   abstract
C-2 Random Error reduction Measures for Earth Sensor Under the Influence of Minute Vibration Interference
       at the Natural Frequency of Its Torsion Bar   abstract
C-3 FUNDAMENTAL STRATEGIES FOR DEPLOYMENT AND LIBRATION CONTROL
       OF A TETHERED SYSTEM IN ELLIPTICAL ORBITS   abstract
C-4 Deployment / Retrieval Control Simulation of a Tethered Satellite with Mass and Flexibility   abstract
C-5 Touch-Down Dynamics of MUSES-C for Asteroid Sampling   abstract
C-6 Landing Phase Simulation of MUSES-C GNC system   abstract
C-7 On the Effects of Gravitational Acceleration for Sample Collection from Minor Body Surfaces   abstract
C-8 Motion Dynamic Simulations and Experiments of an Exploration Rover on Natural Terrain   abstract
C-9 Movement of the Microgravity Rover with a Spring   abstract
C-10 STABILITY OF HOVERING SPACECRAFT ABOVE A SMALL BODY   abstract
C-11 A New Algorithm for Attitude Determination Using Star Tracker   abstract
C-12 Initial Value Setting Efficient for Shape from Shading to Estimate 3-D Terrain   abstract
C-13 Application of Bionics to Imaging Sensor-I   abstract
C-14 Space Robot Reorientation Using Rhythmic Motion Generated by a Brain / Nerve Model   abstract
C-15 Locomotion Control of a Multipod Locomotion Robot using Oscillators   abstract
C-16 Physical Evaluation of Impact Dynamics on a High-Speed Hybrid Motion Simulator   abstract
C-17 A Study on Collision Dynamics of Multi-Rigid-Bodies System   abstract
C-18 System development and ground experiments of a clocking
       mechanism for small mothership-daugtership satellite   abstract
C-20 Development and fundamental experiments of Ground simulation system for Robo-Sat Clusters   abstract
C-21 Image-based Self-Motion Estimation of Hopping Rover   abstract