| 摘要 |
The system (50a) has a motor-driven mechanism (52a) for displacing a thruster (51) on sides of an orbit plane and orienting the thruster so as to control a component perpendicular to the orbit of force to control inclination of the satellite. The mechanism displaces the thruster along an axis parallel to velocity of the satellite and orients the thruster so as to control a component of force on the axis to control orbit, an amplitude and a direction of torque in a plane perpendicular to another axis (F), to control kinetic moment, where the system controls orbital parameters of the satellite. An independent claim is also included for a satellite in earth orbit provided with a propulsion system. |
