Satellite with electromagnetic control of objects

1. A satellite comprising a main body and further comprising, in orbit:

at least one free object floating in space including a portion of a payload transferred from the main body, the free object being restricted to a predetermined position and attitude relative to the main body,

means for generating an electromagnetic force and an electromagnetic torque for controlling the position and the attitude of the free object in accordance with a master-slave relationship.

2. A satellite as claimed in claim 1 wherein said payload portion of the free object is at least one of a mirror type means for reflecting rays in the visible, ultraviolet or infrared, spectrum, and electromagnetic beam transmission antenna for reflecting rays in other regions of the electromagnetic spectrum.

3. A satellite as claimed in claim 1 , wherein said main body includes means for providing a function selected from the group consisting of central computer, backing store and computation power, communication with the Earth, payload other than that portion of said payload on board the free object and associated data processing, data storage, synchronization, FDIR.

4. A satellite as claimed in claim 1 comprising a plurality of free objects and wherein the position of said free objects is controlled by creating a pulsed magnetic field and alternately turning the respective electromagnetic actuators of each free object on and off sufficiently rapidly for the respective inertias of said free objects to render pointing insensitive to such control.

5. A satellite as claimed in claim 1 including a plurality of free objects which, at launch, are stacked with fixing and stacking mechanisms of the electromagnetic locking type.

6. A satellite as claimed in claim 1 wherein:

said free object includes means for locating said free object, at least one first electromagnetic actuator including at least one first electromagnetic coil adapted to generate an electromagnetic force and an electromagnetic torque, at least one magnetometer for measuring local magnetic field information, and means for telecommunication of said local magnetic field information,

said main body includes a central computer for determining the current to be injected into said coil to correct said electromagnetic force and said electromagnetic torque as a function of the required position and of the attitude of the free object.

7. A satellite as claimed in claim 6 wherein said main body itself includes at least one coarse inertial actuator, and at least one electromagnetic actuator including at least one second electromagnetic coil for generating its own electromagnetic force and electromagnetic torque.

8. A satellite as claimed in claim 6 wherein said free object location means include means for receiving information from a star tracker to determine the inertial position of said free object and radio frequency relative positioning means of the GPS type.

9. A satellite as claimed in claim 6 wherein a radio frequency link of said relative positioning means is used as an internal data transmission bus between said main body and said at least one free object.

10. A satellite as claimed in claim 1 wherein a pseudo-satellite is used in free space to absorb onboard increments/decrements of momentum in the main body—free objects satellite system.

11. A satellite as claimed in claim 10 wherein each element of the main body—free objects—pseudo-satellite system is charged with an identical quantity of electrical charge to produce a short-range repulsive force adapted to fade to a negligible level when said elements are at a predetermined distance from each other and not to interfere with the electromagnetic control forces, said charging arrangement generating a short-range passive anticollision system based on electrostatic repulsion.