Satellite Attitude Control System Using a Spherical Reaction Wheel
Guidance Law for Lunar Lander with Input Constraint AIAA Paper
ICAS2014_0730: FORMATION FLIGHT OF FIXED-WING UAVS USING ARTIFICIAL POTENTIAL FIELD
LANDING SYSTEM USING EXTENDED DYNAMIC WINDOW APPROACH FOR FIXED-WING UAV
Orbital Maneuver for Spacecraft Using Generalized Canonical Transformation (AAS 13-791)
Potential study of low pressure exhaust gas recirculation on heavy duty diesel engines
Three-Dimensional Entry Guidance Using Exact Linearization
Tracking Control to Near-Optimal Trajectory for a Lunar Lander
Vector Fields for UAV Guidance Using Potential Function Method for Formation Flight (AIAA 2013-4626)
Development of Three-Dimensional Reaction Wheel Using Spherical Rotor
An Automatic Landing System Using Adaptive Control for a Re-Entry Vehicle
Development of Various Coloring Design Painting Technology for Cars
Guidance Law Based on Bifurcating Velocity Field for Formation Flight
Performance Evaluation of Experimental Device for Space Robot
AUTONOMOUS FORMATION FLIGHT USING BIFURCATING POTENTIAL FIELDS
Proximity Maneuver and Obstacle Avoidance Control Using Potential Function Guidance Method