Workshop on JAXA Astrodynamics and Flight Mechanics, 2009 (July 30-31, 2009. Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan
In this research, a control strategy for a spacecraft("Pursuer") to rendezvous with an uncooperative object ("Target") is dealt with. This strategy consists of a feedforward optimal control phase and feedback control phases. In the feedforward optimal control phase, the pursuer is injected into trajectory synchronized with the target's motion using the future position and velocity of the target obtained by motion estimation. In this paper, designing the optimal control maneuver to the trajectory synchronized with the target motion assuming a space debris removal mission in LEO is investigated.
内容記述
形態: カラー図版あり
内容記述（英）
Physical characteristics: Original contains color illustrations
Relative Motion Estimation and Control Strategy for a Spacecraft to an Uncooperative Object
