Enable a radiating element based on an orientation signal
US-10651552-B2 · May 12, 2020 · US
US11822004B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11822004-B2 |
| Application number | US-202017102817-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 24, 2020 |
| Priority date | Nov 27, 2019 |
| Publication date | Nov 21, 2023 |
| Grant date | Nov 21, 2023 |
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A radar, flying device including such a radar, processing method in a radar embedded in a flying device and associated computer program are disclosed. In one aspect, the radar includes a transceiver antenna including a plurality of radiating elements configured to transmit and receive an electromagnetic wave. The radar includes an antenna gain control unit, by activating/inhibiting radiating elements, in transmission and/or reception configured to keep the reception level of an electromagnetic wave below a determined threshold below the saturation zone of the antenna, as well as by activating/inhibiting radiating elements in reception, configured to compensate the amplitude variation of the ground/sea clutter, over the duration of the reception.
Opening claim text (preview).
What is claimed is: 1. A radar comprising: a transceiver antenna including a plurality of radiating elements distributed over a surface and configured to transmit and receive an electromagnetic wave; an antenna gain control unit, wherein the antenna gain control unit is configured to feedback control, through an adjustment loop, the antenna gain in transmission and/or reception by turning on or off radiating elements of the plurality of radiating elements, in order to keep the reception level of the electromagnetic waves below a determined threshold below the saturation zone of the radar, and wherein the antenna is further configured to emit from a given height relative to a given surface and at a given incidence angle, the gain control unit is configured, in the adjustment loop, to perform at least one of the following operations: determining the deviation between the current level of the received electromagnetic wave and a reference level, in order to determine the gain adjustment as a function of the deviation and to command the turning off or on of radiating elements in transmission and/or reception based on the determined gain adjustment, and determining at least one set of value(s) comprising at least one value among the given height and the given incidence angle, in order to determine the gain adjustment based on each value of the determined set of value(s) and to command the turning off or on of radiating elements in transmission and/or reception based on the determined gain adjustment. 2. The radar according to claim 1 , wherein the gain control unit is further configured, in the adjustment loop, to adjust the gain according to a function calculating the gain value based on at least each value of the set of value(s), the function being a decreasing function of the value when the value is the height and an increasing function of the value when the value is the incidence angle. 3. The radar according to claim 1 , wherein the gain control unit is further configured to modify the gain according to at least one operation among a nonzero power modification command emitted by each radiating element and a command to turn on or off at least some of the radiating elements. 4. The radar according to claim 1 , further comprising: a compensating module configured to attenuate the amplitude of a received electromagnetic wave based on the distance traveled to the surface by the electromagnetic wave, the compensating module being configured to perform this attenuation on digital samples of the received electromagnetic waves based on the distance and/or to perform the attenuation by a command to turn on or off at least some of the radiating elements determined based on the distance. 5. A flying device comprising an embedded radar according to one of the preceding claims. 6. A processing method in a radar embedded in a flying device, the radar comprising a transceiver antenna including a plurality of radiating elements distributed over a surface and configured to transmit and receive an electromagnetic wave, the method comprising: transmitting an electromagnetic wave from the antenna and receiving an electromagnetic wave by the antenna; wherein the method comprises the following implemented by an electronic gain control unit of the radar: feedback controlling, through an adjustment loop, the antenna gain in transmission and/or reception by turning on or off radiating elements of the plurality of radiating elements, in order to keep the reception level of the electromagnetic waves below a determined threshold below the saturation zone of the radar, wherein the adjustment loop comprises at least one of a and b: a) determining the deviation between the current level of the received electromagnetic wave and a reference level, determining the gain adjustment as a function of the deviation and commanding the turning off or on of radiating elements in transmission and/or reception based on the determined gain adjustment; and b) the transmission having taken place from a given height relative to a given surface and at a given incidence angle, determining at least one set of value(s) comprising at least one value among the given height and the given incidence angle, determining the gain adjustment based on each value of the determined set of value(s) and commanding the turning off or on of radiating elements in transmission and/or reception based on the determined gain adjustment. 7. The processing method in an embedded radar according to claim 6 , wherein the adjustment loop comprises adjusting the gain according to a function calculating the gain value based on at least each value of the set of value(s), the function being a decreasing function of the value when the value is the height and an increasing function of the value when the value is the incidence angle. 8. A computer program comprising software instructions which, when executed by a computer, carry out a method according to claim 6 .
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