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
Practical rendezvous problems must be treated under practical conditions such as the limitation of thruster activation direction, the sensor FOV, the sun direction, etc. We treat rendezvous trajectory planning with such practical constrained conditions by using a new approach to achieve nonlinear control with respect to a known control Lyapunov function (CLF), and constrained control value conditions.
内容記述
形態: カラー図版あり
内容記述(英)
Physical characteristics: Original contains color illustrations