Low side lobe level AESA hybrid fate / ensemble calibration
A calibration system for AESAs induces the AESA to produce a far field radiation pattern while near field measurements are taken; an initial calibration is produced, and complex aperture holograms are calculated. Based on the complex holograms, phase and amplitude error maps are computed. T/R module amplitude and phase are then adjusted to compensate for the error map. The system evaluates the refined far field radiation pattern to iteratively recompute complex aperture excitations to realize adequate far field performance and new hologram error maps until a desired level of precision is reached.
1 . A computer apparatus comprising:
one or more sensors disposed proximal to an ESA antenna in a near field range test environment to directly receive signals from radiating elements of the ESA antenna; and
at least one processor in data communication with a memory storing processor executable code for configuring the at least one processor to:
drive radiating elements in an electronically scanned array (ESA) antenna being calibrated when the ESA is in a transmit mode;
receive signals from the one or more sensors based on the driven radiating elements when the ESA is in a receive mode;
calculate far field calibration coefficients for each of the radiating elements;
calculate one or more error maps corresponding to a face of the ESA antenna being calibrated;
determine amplitude and phase adjustments for one or more T/R modules in the ESA being calibrated;
apply the amplitude and phase adjustments to the one or more T/R modules in the ESA being calibrated; and
recalculate far field calibration coefficients for each of the radiating elements to produce a calibrated ESA antenna to a desired far field radiation pattern.
2 . The computer apparatus of claim 1 , wherein the amplitude and phase adjustments recalculated far field calibration coefficients produce side lobe levels of less than −30 dBp in the receive mode.
3 . The computer apparatus of claim 1 , wherein the at least one processor is further configured to iteratively recalculate aperture amplitude and phase or delay calibration coefficients and redetermine amplitude and phase adjustments until a threshold precision is reached for desired far field performance.
4 . The computer apparatus of claim 3 , wherein the threshold precision is defined by a far field null depth, width, and azimuthal and elevation location.
5 . The computer apparatus of claim 1 , wherein the error maps are defined by complex aperture holograms.
6 . The computer apparatus of claim 1 , wherein the ESA antenna being calibrated is disposed in a near field range test environment.
7 . A method comprising:
driving radiating elements in an electronically scanned array (ESA) antenna being calibrated;
receiving signals based on the driven radiating elements;
calculating far field calibration coefficients for each of the radiating elements;
calculating one or more error maps corresponding to a face of the ESA antenna being calibrated;
determining amplitude and phase adjustments for one or more T/R modules in the ESA being calibrated;
applying the amplitude and phase adjustments to the one or more T/R modules in the ESA being calibrated while in a transmit mode; and
recalculating far field calibration coefficients for each of the radiating elements to produce a calibrated ESA antenna to a desired far field radiation pattern.
8 . The method of claim 7 , wherein the amplitude and phase adjustments recalculated far field calibration coefficients produce far field nulls.
9 . The method of claim 8 , wherein a threshold precision is defined by a far field null depth, width, and azimuthal and elevation location.
10 . The method of claim 7 , further comprising iteratively recalculating far field calibration coefficients and redetermining amplitude and phase adjustments until a threshold precision is reached.
11 . The method of claim 7 , wherein the error maps are defined by complex aperture holograms.
12 . The method of claim 7 , wherein the ESA antenna being calibrated is disposed in a near field range test environment.
13 . An antenna calibration system comprising:
a near field range test environment;
one or more sensors disposed in the near field range test environment; and
at least one processor in data communication with a memory storing processor executable code for configuring the at least one processor to:
drive radiating elements in an electronically scanned array (ESA) antenna being calibrated when in a transmit mode;
receive signals from the one or more sensors based on the driven radiating elements when the ESA is in a receive mode;
calculate complex aperture calibration coefficients for each of the radiating elements;
calculate one or more error maps corresponding to a face of the ESA antenna being calibrated;
determine amplitude and phase adjustments for one or more T/R modules in the ESA being calibrated;
apply the amplitude and phase adjustments to the one or more T/R modules in the ESA being calibrated; and
recalculate far field calibration coefficients for each of the radiating elements to produce a calibrated ESA antenna to a desired far field radiation pattern.
14 . The antenna calibration system of claim 13 , wherein the amplitude and phase adjustments recalculated far field calibration coefficients produce far field nulls according to desired width, depth, and azimuthal and elevation location.
15 . The antenna calibration system of claim 13 , wherein the at least one processor is further configured to iteratively recalculate far field calibration coefficients and redetermine amplitude and phase adjustments until a threshold precision is reached.
16 . The antenna calibration system of claim 15 , wherein the threshold precision is defined by a desired side lobe level.
17 . The antenna calibration system of claim 13 , wherein the error maps are defined by complex aperture holograms.