Accurate Landmark Tracking for Navigating Hayabusa Prior to Final Descent (AAS 06-215)
A Control Configured Small Circular Halo Orbit Around L2 (AAS 05-425)
A Design of Small Circular Halo Orbits around the L2 of the Earth-Moon System (AAS 12-539)
An Attempt for Regularization and Formation Flight Expression Along Two-Body Motion (AAS 08-140)
A New Attitude Maneuver Using Kinematics and Dynamics of Non-Holonomic Turn (AAS 06-100)
A New Guidance Strategy in Aerodynamic Ascent Path Using Air-Breathing Propulsion (AAS 05-350)
A Scheme for Simplified Trajectory Design in Aero-Gravity Assist Using Singular Orbits (AAS 13-498)
A Study on the Guidance Correcting Law for the Aerodynamic Ascent Flight (AAS 04-149)
Attitude Control of Spinning Solar Sail with Huge Membrane (AAS 08-221)
Autonomous Descent and Touch-Down Via Optical Sensors (AAS 01-134)
Development of a Target Marker for Landing on Asteroids (AAS 00-171)
Guidance and Navigation Operation for Rehearsals and Touch-Downs in Hayabusa (AAS 06-183)
Guidance and Navigation Strategy Based Only on the Range Measurement (AAS 03-530)
Hayabusa's Touching-Down to Itokawa - Autonomous Guidance and Navigation (AAS 06-214)
Ion Engines Cruise of Hayabusa to Itokawa - Trajectory Synthesis and Results (AAS 06-209)
Low-Thrust Transfer Between Jovian Moons Using Manifolds (AAS 11-235)
Mission Analysis of Near Earth Asteroid Exploration by Miniature Asteroid Interceptors (AAS 06-212)
Mission Analysis of the Sample Return From Primitive Type Near Earth Asteroid (AAS 07-246)
MUSES-C Launch and Early Orbit Operations Report (AAS 03-662)
On Ballistic Acquisition of Short Period Out-of-Ecliptic Trajectories (AAS 09-339)
On Single-Wheel Configured Spacecraft and the Attitude Stability Revisited (AAS 08-139)
On the Deployment and Collision Avoidance Strategy for Formation Flight (AAS 03-384)
On the Multiple Sample and Return Opportunities From Near Earth Asteroids (AAS 01-153)
On the Relation Between the Local Formation Control Law and the Resulted Configuration (AAS 04-263)
Optical Hybrid Navigation in Hayabusa - Approach, Station Keeping and Hovering (AAS 06-210)
Orbit Control Method for Solar Sail Demonstrator IKAROS Via Spin Rate Control (AAS 11-633)
Orbit Determination for Nozomi (AAS 01-103)
Orbit Expressions in the Continuous Polar Coordinate System (AAS 12-519)
Preparatory Study: Accessing Asteroids on Horseshoe Orbits (AAS 13-935)
Resonant Stability and its Criterion for the Orbits Around the Sphere of Influence (AAS 01-224)
Return of Hayabusa Spacecraft and Reentry of Its Capsule (AAS 11-058)
Robotic Lander Minerva, Its Mobility and Surface Exploration (AAS 01-136)
Solar Sail Attitude Dynamics Considering Sail Deformation (AAS 13-759)