ICAS2016_0195: MINIMUM-TIME FORMATION USING OPTIMAL SOLUTIONS OF SINGLE FIXED-WING AIRCRAFT
Minimum Energy Steering Law for Tracking Maneuvers of Satellites with CMGs (AAS 12-514)
Minimum Energy Controller for Large Attitude Maneuver by Two Wheels
The examination of the method to predict life of vibration absorbency
3-Dimensional Near-Minimum Fuel Guidance Law of a Lunar Landing Module
Minimum Fuel Trajectories to Elliptic Orbits Using Solar Electric Propulsion (AAS 03-387)
Minimum Fuel Trajectories for Sample-Return Mission Using Solar Electric Propulsion (AAS 01-516)
Optimal Controller for a Space Platform Based Manipulator Capturing a Satellite
Minimum Fuel Trajectories for Sample-Return Mission Using Solar Electric Propulsion (AAS 01-516)
Experiments on Space Robot Path Planning Using the Sensors Database, Part II