High bandwidth data transfer
A data delivery system has a tether deployable from an aircraft having a first data repository, a transmission pod at a deployed end of the tether, the transmission pod having first wireless communication circuitry, a communication conductor in parallel with the tether connecting the data repository in the aircraft with the first wireless communication circuitry in the transmission pod, and a receiving station on ground surface having a receiving antenna, second wireless communication circuitry compatible with the first wireless communication circuitry in the transmission pod, and a second data repository. The tether is deployed from the aircraft in a manner to position the transmission pod stationary proximate the receiving station antenna, and data is downloaded from the data repository in the aircraft to the data repository in the receiving station via the communication conductor and the wireless communication circuitry in the transmission pod.
1. A data transfer system, comprising:
a tether deployable from an aircraft having a first data repository;
a transmission pod at a deployed end of the tether, the transmission pod having first wireless communication circuitry;
a communication conductor in parallel with the tether connecting the data repository in the aircraft with the first wireless communication circuitry in the transmission pod; and
a receiving station on ground surface having a receiving antenna, second wireless communication circuitry compatible with the first wireless communication circuitry in the transmission pod, and a second data repository;
wherein the tether is configured to be deployed from the aircraft in a manner to position the transmission pod stationary proximate the receiving station antenna, and data is configured to be transferred between the data repository in the aircraft and the data repository in the receiving station via the communication conductor and the wireless communication circuitry in the transmission pod.
2. The data transfer system of claim 1 wherein the aircraft is a helicopter, and the pod is configured to be positioned by deploying the tether and maneuvering the helicopter to be directly over the receiving station.
3. The data transfer system of claim 1 wherein the aircraft is a fixed wing aircraft, and the pod is configured to be positioned by piloting the fixed wing aircraft in a circular orbit at a position, an orbit diameter, and a speed that positions the transmission pod proximate the receiving station antenna.
4. The data transfer system of claim 1 further comprising an end effector having controllable thrusters at the deployed end of the tether along with the transmission pod, wherein the thrusters are configured to be controlled to position the transmission pod proximate the receiving station antenna.
5. The data transfer system of claim 4 further comprising an imaging device incorporated in the end effector, configured to transmit image data via the communication conductor parallel with the tether from the imaging device back to the aircraft.
6. The data transfer system of claim 5 further comprising a display in the aircraft configured to display the image data to an operative, and control circuitry configured to enable the operative to control the thrusters of the end effector, wherein the end effector is configured to be piloted by the operative to approach and remain proximate the receiving station antenna.
7. The data transfer system of claim 1 wherein the aircraft is a surveillance aircraft with image data stored in the data repository in the aircraft.
8. A data transfer method, comprising:
deploying a tether having a communication pod with first wireless communication circuitry at a deployable end from an aircraft having a first data repository, the first data repository and the wireless communication circuitry in the transmission pod connected by a conductor in parallel with the tether;
positioning the communication pod stationary proximate a receiving antenna at a receiving station having a second data repository; and
transferring data between the data repository in the aircraft to the data repository in the receiving station via the communication conductor and the wireless communication circuitry in the transmission pod.
9. The data delivery method of claim 8 wherein the aircraft is a helicopter, comprising positioning the pod by deploying the tether and maneuvering the helicopter to be directly over the receiving station.
10. The data delivery method of claim 8 wherein the aircraft is a fixed wing aircraft, comprising positioning the transmission pod by piloting the fixed wing aircraft in a circular orbit at a position, an orbit diameter, and a speed that positions the transmission pod proximate the receiving station antenna.
11. The data delivery method of claim 8 further comprising an end effector having controllable thrusters at the deployed end of the tether along with the transmission pod, comprising controlling the thrusters to position the transmission pod proximate the receiving station antenna.
12. The data delivery system of claim 11 further comprising an imaging device incorporated in the end effector, comprising transmitting image data via the communication conductor parallel with the tether from the imaging device back to the aircraft.
13. The data delivery method of claim 12 further comprising a display in the aircraft displaying the image data to an operative, and control circuitry enabling the operative to control the thrusters of the end effector, comprising the operative piloting the end effector to approach and remain proximate the receiving station antenna.
14. The data delivery method of claim 8 wherein the aircraft is a surveillance aircraft with image data stored in the first data repository in the aircraft, comprising downloading the image data stored in the first data repository in the aircraft to the second data repository in the receiving station.