High bandwidth optical links for micro-satellite support

1. A high bandwidth satellite downlink communication system comprising:

an onboard tracking detector, installed in a satellite, that detects a position of an incoming optical beam from a first ground station of one or more ground stations;

tracker electronics that determines orientation information of the incoming optical beam based on the position;

control electronics that receive the orientation information from the tracker electronics, and control a waveguide drive electronics based on the orientation information;

the waveguide drive electronics that controls a voltage provided to an electro-optic waveguide beam steering device; and

the electro-optic waveguide beam steering device that steers an outgoing optical beam from the satellite to one of the one or more ground stations based on the voltage, wherein the electro-optic waveguide beam steering device steers the outgoing optical beam by applying the voltage to an electrode having an interface to a beam propagation direction, and wherein as voltage is applied, an index under the electrode is changed relative to a surrounding area and the outgoing optical beam is steered via Snell's law refraction.

2. The system of claim 1 , wherein the tracking detector comprises an on quadrant avalanche photodiode tracking detector.

3. The system of claim 1 , further comprising a receiver aperture lens that focuses the incoming optical beam onto the tracking detector.

4. The system of claim 1 , wherein the electro-optic waveguide beam steering device provides 2-axis control over a field of view.

5. The system of claim 1 , wherein the outgoing optical beam is continuously steered and locked onto the one of the one or more ground stations.

6. The system of claim 1 , wherein the electro-optic waveguide beam steering device further enables free space optical (FSO) communications by steering the outgoing optical beam to one or more moving vehicles within a theater area.

7. A method for steering an optical beam on a satellite comprising:

detecting, on a satellite, a position of an incoming optical beam from a first ground station of one or more ground stations;

determining orientation information of the incoming optical beam based on the position;

receiving the orientation information and controlling a waveguide drive electronics based on the orientation information;

controlling, via the waveguide drive electronics, a voltage that is provided to an electro-optic waveguide beam steering device; and

steering, via the electro-optic waveguide beam steering device, an outgoing optical beam from the satellite to one of the one or more ground stations based on the voltage, wherein the steering comprises applying the voltage to an electrode having an interface to a beam propagation direction, and wherein as voltage is applied, an index under the electrode is changed relative to a surrounding area and the outgoing optical beam is steered via Snell's law refraction.

8. The method of claim 7 , wherein the detecting is performed by a quadrant avalanche photodiode tracking detector.

9. The method of claim 7 , further comprising focusing, via a receiver aperture lens, the incoming optical beam onto the tracking detector.

10. The method of claim 7 , wherein the electro-optic waveguide beam steering device provides 2-axis control over a field of view.

11. The method of claim 7 , further comprising continuously steered and locking the outgoing optical beam onto the one of the one or more ground stations.

12. The method of claim 7 , further comprising the electro-optic waveguide beam steering device enabling free space optical (FSO) communications by steering the outgoing optical beam to one or more moving vehicles within a theater area.