Manifold calibration for a communication system
View Patent ↗A method and apparatus for determining stream weights is provided herein. During operation, an uplink direction of arrival (DOA) and a downlink direction of departure (DOD) calibration procedure is implemented using uplink signals and GPS information from a subset of mobiles without the need of calibration circuitry at the base. Because the presented calibration procedure needs no new hardware it can be deployed in existing deployments with only a soft-ware upgrade.
1. A method for performing direction of arrival (DOA) manifold calibration, the method comprising the steps of:
determining by a base station, an angle θ to a mobile unit, wherein the determination is made by a technique other than determining a direction of a signal received from the mobile unit;
receiving by the base station, an uplink transmission (Y(k,b)) from the mobile unit, wherein k is a subcarrier index and b is a time index;
determining, by the base station, a dominant vector r(b) from the received uplink transmission;
computing, by the base station, calibration coefficients C(b) based on the angle θ and r(b) and wherein computing the calibration coefficients comprises the steps of:
determining W=diag(r(b)); and
determining C(b)=diag(ĉ b ), where ĉ b =(W H W) −1 W H a(θ), where a (θ)
is an array manifold vector; and
applying, by the base station, the calibration coefficients to received uplink transmissions.
2. The method of claim 1 wherein the step of determining the angle θ is accomplished by receiving GPS information from the mobile unit.
3. The method of claim 1 wherein the effect of outdated DOA calibration coefficients is removed from the dominant vector r(b).
4. A method for performing direction of departure (DOD) manifold calibration, the method comprising the steps of:
determining by a base station, an angle θ to a mobile unit, wherein the determination is made by a technique other than determining a direction of a signal received from the mobile unit;
receiving by the base station, feedback from the mobile unit regarding a dominant downlink vector r(b), wherein b is a time index;
determining, by the base station, calibration coefficients D based on the angle θ and dominant downlink vector r(b), wherein the step of determining the calibration coefficients D, comprises the steps of:
determining W=diag(r(b)); and
determining D=diag({circumflex over (d)} b ), where {circumflex over (d)} b =(W H W) −1 W H a(θ), where a(θ) is
an array manifold vector; and
applying, by the base station, the calibration coefficients to downlink transmissions to the mobile unit.
5. The method of claim 4 wherein the step of determining the angle θ is accomplished by receiving GPS information from the mobile unit or obtaining time-of-arrival information concerning the mobile unit.
6. The method of claim 4 wherein the effect of outdated calibration coefficients is removed from the dominant downlink vector r(b) before calculating the calibration coefficients.
7. An apparatus for performing direction of arrival (DOA) manifold calibration, the apparatus comprising:
calibration circuitry having as an input, information on an angle θ to a mobile unit, an uplink transmission (Y(k,b)) from a mobile unit, wherein k is a subcarrier index and b is a time index, the calibration circuitry determining a dominant vector r(b) from the received uplink transmission, the calibration circuitry outputting calibration coefficients C(b) based on the angle θ and r(b) and wherein the calibration coefficients C(b) are computed by the calibration circuitry based on the angle θ and R(b)r(b) by:
determining W=diag(r(b)); and
determining C(b)=diag(ĉ b ), where ĉ b =(W H W) −1 W H a(θ), where a(θ) is an array manifold vector; and
multiplication circuitry applying the calibration coefficients to received uplink transmissions.
8. The apparatus of claim 7 wherein the information on angle θ comprises GPS information received from the mobile unit.
9. The apparatus of claim 7 wherein the effect of outdated DOA calibration coefficients is removed from the dominant vector r(b).
10. An apparatus for performing direction of departure (DOD) manifold calibration, the apparatus comprising:
calibration circuitry receiving information on an angle θ to a mobile unit and receiving vector feedback from the mobile unit regarding a dominant downlink vector r(b), wherein b is a time index, the calibration circuitry outputting calibration coefficients D based on the angle θ and dominant downlink vector r(b) wherein the calibration coefficients D, are computed by the calibration circuitry by:
determining W=diag(r(b)); and
determining D=diag({circumflex over (d)} b ), where {circumflex over (d)} b =(W H W) −1 W H a(θ), where a (θ) is an
array manifold vector; and
multiplication circuitry applying the calibration coefficients to downlink transmissions to the mobile unit.
11. The apparatus of claim 10 wherein the information on the angle θ comprises GPS information received from the mobile unit.
12. The apparatus of claim 10 wherein the effect of outdated calibration coefficients is removed from the dominant downlink vector r(b) before calculating the calibration coefficients.