Adaptive doppler-nulling digitization for high-resolution
A system includes a transmitter node and a receiver node. Each node of the transmitter node and the receiver node are time synchronized to apply Doppler corrections associated with said node's own motions relative to a stationary common inertial reference frame. The stationary common inertial reference frame is known to the transmitter node and the receiver node prior to the transmitter node transmitting a plurality of signals to the receiver node and prior to the receiver node receiving the plurality of signals from the transmitter node. The receiver node performs adaptive digitization of the signals to account for a speed of the platform.
1. A system comprising:
a transmitter node and a receiver node, wherein each node of the transmitter node and the receiver node comprises:
a communications interface comprising at least one antenna element; and
a controller operatively coupled to the communications interface, the controller including one or more processors, wherein the controller has information of own node velocity and own node orientation;
wherein each node of the transmitter node and the receiver node are time synchronized to apply Doppler corrections associated with said node's own motions relative to a stationary common inertial reference frame;
wherein the stationary common inertial reference frame is known to the transmitter node and the receiver node prior to the transmitter node transmitting a plurality of signals to the receiver node and prior to the receiver node receiving the plurality of signals from the transmitter node;
wherein the receiver node is configured to digitize the plurality of signals using a step size, determine a modulation amplitude of the plurality of signals, and adjust the step size based on the modulation amplitude.
2. The system of claim 1 , wherein the modulation amplitude is based on said node's own motions of the receiver node and the transmitter node.
3. The system of claim 2 , wherein a doppler shift of the plurality of signals is between 1 Hz and 10 MHz.
4. The system of claim 1 , wherein the receiver node is configured to iteratively digitize the plurality of signals using the step size, determine the modulation amplitude of the plurality of signals, and adjust the step size based on the modulation amplitude.
5. The system of claim 1 , wherein one of the receiver node or the transmitter node is a low-earth orbit satellite.
6. The system of claim 1 , wherein the transmitter node is configured to adjust a transmit frequency according to an own speed and an own velocity direction of the transmitter node so as to perform a transmitter-side Doppler correction; wherein the receiver node is configured to adjust a receiver frequency of the receiver node according to the own node velocity and the own node orientation so as to perform a receiver-side Doppler correction.
7. The system of claim 6 , wherein an amount of adjustment of the adjusted transmit frequency is proportional to a transmitter node velocity projection onto a Doppler null direction, wherein an amount of adjustment of the adjusted receiver frequency is proportional to a receiver node velocity projection onto the Doppler null direction.
8. The system of claim 7 , wherein the receiver node is configured to determine a relative speed between the transmitter node and the receiver node.
9. The system of claim 8 , wherein the receiver node is configured to determine a direction that the transmitter node is in motion and a velocity vector of the transmitter node.
10. The system of claim 1 , wherein the stationary common inertial reference frame is a two-dimensional (2D) stationary common inertial reference frame.
11. The system of claim 1 , wherein the stationary common inertial reference frame is a three-dimensional (3D) stationary common inertial reference frame.
12. The system of claim 1 , wherein the at least one antenna element comprises at least one of at least one directional antenna element or at least one omnidirectional antenna element.
13. A receiver node comprising:
a communications interface comprising at least one antenna element; and
a controller operatively coupled to the communications interface, the controller including one or more processors, wherein the controller has information of own node velocity and own node orientation;
wherein the receiver node is time synchronized with a transmitter node to apply Doppler corrections associated with said node's own motions relative to a stationary common inertial reference frame;
wherein the stationary common inertial reference frame is known to the transmitter node and the receiver node prior to the transmitter node transmitting a plurality of signals to the receiver node and prior to the receiver node receiving the plurality of signals from the transmitter node;
wherein the receiver node is configured to digitize the plurality of signals using a step size, determine a modulation amplitude of the plurality of signals, and adjust the step size based on the modulation amplitude.
14. The receiver node of claim 13 , wherein the modulation amplitude is based on said node's own motions of the receiver node and the transmitter node.
15. The receiver node of claim 14 , wherein a doppler shift of the plurality of signals is between 1 Hz and 10 MHz.
16. The receiver node of claim 13 , wherein the receiver node is configured to iteratively digitize the plurality of signals using the step size, determine the modulation amplitude of the plurality of signals, and adjust the step size based on the modulation amplitude.
17. The receiver node of claim 13 , wherein the transmitter node is configured to adjust a transmit frequency according to an own speed and an own velocity direction of the transmitter node so as to perform a transmitter-side Doppler correction; wherein the receiver node is configured to adjust a receiver frequency of the receiver node according to the own node velocity and the own node orientation so as to perform a receiver-side Doppler correction.
18. The receiver node of claim 17 , wherein an amount of adjustment of the adjusted transmit frequency is proportional to a transmitter node velocity projection onto a Doppler null direction, wherein an amount of adjustment of the adjusted receiver frequency is proportional to a receiver node velocity projection onto the Doppler null direction.
19. The receiver node of claim 18 , wherein the receiver node is configured to determine a relative speed between the transmitter node and the receiver node.
20. The receiver node of claim 19 , wherein the receiver node is configured to determine a direction that the transmitter node is in motion and a velocity vector of the transmitter node.