1. Field of the Invention
The present invention relates to improving transmitted signal quality in an active phased array antenna utilizing solid state power amplifiers transmitting two or more fundamental communications beams. In particular, selected intermodulation beams arising from nonlinear amplifier operation are nulled to improve signal quality.
2. Discussion of the Related Art
Active phased array antennas include a plurality of radiators driven by respective amplifiers.
As used herein, the term processor refers to a device for processing information. In particular, digital processors such as microprocessors and other digital processing devices are included. Various processor embodiments include one or more processors. And, some processor embodiments include one or more memory device(s) such as semiconductor and/or hard disc drive memory devices and input/output device(s) such as bus communications, parallel communications, and serial communications devices.
Beam forming section inputs include a plurality of signals 224 and their related angles 222. For each signal S1, S2, two angles, commanded elevation θ0 and azimuth φ0 determine the direction of the beam carrying the signal and therefore the intended receiver of the signal. For example, a first fundamental beam might be directed to a receiver in a first city at the angle pair (θ0, φ0) and a second fundamental beam might be directed to another receiver in another city at the angle pair (θ′0, φ′0). Manipulating the direction of a communication beam is sometimes referred to as steering the beam.
Beam forming entails creation of a phase front for each beam that is normal to the desired direction of the beam. These phase fronts are created by appropriately shifting the phases of the incoming signals S1, S2 in beam forming elements 204. Each one of “i” antenna beam forming elements includes steering phase shifters PSi1, PSi2 that create corresponding shifted signals Si1a, Si2a. In various embodiments, the phase shifters include one or both of digital and analog phase shifters.
Phase shifts Zi1, Zi2 are applied to the signals S1, S2 to create shifted signals Si1a, Si2a. In an embodiment, the phase shifts are calculated within the fundamental beam steering processor 202. And, in an embodiment, these applied phase shifts are functions of uniform progressive phases αx, αy as shown in equations 1a,b below.
Z
i1
=q
1(α1,x, α1,y) Equation 1a
Z
i2
=q
2(α′1,x,α′1,y) Equation 1b
As shown in equations 2a-d below, the uniform progressive phases αxx, αy are determined by the commanded beam angle pairs θ0, φ0 and θ′0, φ′0.
Note, equations 2a-d assume dx=dy=d. This assumption simplifies the analysis and the equations.
Phase shifter outputs Si1a and Si2a are combined and amplified in the ith feed chain element 205 that includes a signal combiner 210 and a solid state amplifier 212. The signal combiner 210 is coupled to the input signals Si1a, Si2a and its output 211 is amplified in the amplifier. The ith radiator element 220 is coupled to the amplifier 212 via an amplifier output 213.
A phased array antenna system includes phase shifters for nulling selected intermodulation beams. In an embodiment, a nulling section is interposed between a beam forming section and a feed chain section and an antenna has a plurality of radiators, each radiator being coupled to a respective amplifier in the feed chain section. Each amplifier is coupled to a respective nulling phase shifter in the nulling section and each nulling phase shifter is coupled to a respective steering phase shifter in the beam forming section. One or more processors are for activating the phase shifters. The phased array antenna system is operative to simultaneously transmit a plurality of signals to respective locations.
In an embodiment, the phased array antenna system includes one or more processors for calculating directivity patterns and one or more memory devices for storing calculated directivity patterns. A signal sampler is for sampling fundamental and intermodulation forward and reflected traveling wave signal levels at the input of each radiator and one or more processors are for updating the stored directivity patterns in accordance with the sample values.
In an embodiment a single processor is used. And, in an embodiment, the beam forming section includes a processor and the nulling section includes a processor.
The present invention is described with reference to the accompanying figures. These figures, incorporated herein and forming part of the specification, illustrate embodiments of the invention and, together with the description, further serve to explain its principles enabling a person skilled in the relevant art to make and use the invention.
The disclosure provided in the following pages describes examples of some embodiments of the invention. The designs, figures, and descriptions are non-limiting examples of the embodiments they disclose. For example, other embodiments of the disclosed device and/or method may or may not include the features described herein. Moreover, disclosed advantages and benefits may apply only to certain embodiments of the invention and should not be used to limit the disclosed invention.
As used herein, the term “coupled” includes direct and indirect connections. Moreover, where first and second devices are coupled, other devices including active devices may be interposed between them.
A nulling section incorporating “i” nulling elements 352 is coupled with commanded angle inputs 322. Signals with an applied phase shift for beam steering are outputs 351 of the beam forming section and are coupled to the nulling section 352. Nulling section outputs 353 are coupled with a feed chain section incorporating “i” feed chain elements 354. The feed chain section is coupled 355 with “i” radiators 320 of an antenna array 360.
A comparison of
During operation of the invention's nulling function, attenuators ATi1, ATi2 are used to equalize radiator amplitudes by applying suitable attenuations A11, A12, A21, A22 . . . AM1, AM2 (where M represents the number of elements in the array) and nulling phase shifters PNi1, PNi2 are used to apply a nulling phase distribution. In various embodiments, the phase shifters include one or both of digital and analog phase shifters. Because it is not always beneficial to operate this nulling functionality, embodiments of the invention adapt by selectively operating the nulling function.
When the nulling function is not in operation, a) attenuators ATi1, ATi2 apply a uniform attenuation to signals such that A11=A21= . . . AM1=A12=A22= . . . =AM2=0 and b) nulling phase shifters PNi1, PNi2 apply a uniform phase distribution to signals such that β11=β21= . . . =βM1=β12=β22= . . . =βM2=0. Adaptive functionality is discussed further below, after operation of the nulling phase shifters has been described.
In the nulling section 352, the once shifted signals Si1a, Si2a are attenuated by respective attenuators ATi1, ATi2 to equalize their levels. Nulling phase shifters PNi1, PNi2 are provided to process the attenuated signals 362, 364 creating twice shifted signals Si1b, Si2b. One or more processors perform these functions. In an embodiment, an intermodulation beam nulling processor 361 is coupled to the commanded angle signals 322 and provides a) attenuating outputs Ai1, Ai2 coupled to respective attenuators ATi1, ATi2 and b) phase shifting outputs βi1, βi2 coupled to respective phase shifters PNi1, PNi2.
Nulling unwanted intermodulation beams (“IM” beam or “IMB”) entails applying a nulling phase distribution to signals passing through the nulling section 352. The nulling phase distribution shifts the phases of all of the signals Si1a, Si2a by a nulling angle βu,i with a magnitude of 90/N degrees where N is the order of the intermodulation beam to be nulled. See the appendix to this specification for further explanation of these nulling phase shifts.
Referring to βu,i as the nulling phase change for the uth signal and the ith array element, in an exemplary 3×3 phased array antenna, the nulling phase distribution (in degrees) for the first signal is below.
Similarly, the nulling phase distribution for the second signal is below.
These nulling phase distributions have a “checkerboard” type pattern where each successive element has a phase shift of equal magnitude but of opposite sign.
In some embodiments, a single set of phase shifters applies both the steering and the nulling phase shifts. In these embodiments, the steering phase shifts Zi1, Zi2 are added to the respective nulling phase shifts βi1, βi2 and the combined shifts are applied to respective phase shifters. For example, the phase shifts can be combined in a single processor carrying out the functions of the fundamental beam steering processor 202 and the intermodulation beam nulling processor 359.
Turning now to the question of whether nulling phase distributions should be applied, a means for comparing the attenuation of fundamental beams (undesirable) and the attenuation of intermodulation beams (desirable) is required. For example, if application of the nulling phase distribution increases the directivity of selected intermodulation beam(s) while the corresponding fundamental beam is little changed, the application is detrimental.
As shown in Section 2.0 of the appendix, the directivity D of a beam depends on the complex (amplitude and phase) excitation of the mnth element designated Imn, elevation and azimuth angles (θ, φ), and the spacing between rows dx and columns dy of the phased array. In particular, the peak directivity of the fundamental beams can be expressed as functions of these variables.
D
1st fundamental beam
=D1F=D(Imn,θ0,φ0,dx,dy) Equation 3a
D
2nd fundamental beam
=D2F =D(I′mn,θ′0,φ′0,dx,dy) Equation 3b
The peak directivity of the intermodulation beams of a selected order N also depends on these variables. In particular, the values of progressive phases (αN,x, αN,y, α′N,x, α′N,y) corresponding to an Nth order intermodulation beam are calculated as indicated below.
To obtain the related intermodulation beam elevation and azimuth scan angles (θN,0, φN,0, θ′N,0, φ′N,0), the progressive phase values of equations 4a-d are used in Equations 5a-c (similar to Equations 2a-c) to solve for these values.
Note, equations 5a-d assume dx=dy=d. This assumption simplifies the analysis and the equations.
Peak directivity of the intermodulation beams is calculated using the directivity equation discussed above.
D
1st intermodulation beam
=D1I=D(Imn,θN,φN,dx,dy) Equation 6a
D
2nd intermodulation beam
=D2I=D(I′mn,θN′,φN′,dx,dy) Equation 6b
Directivities before and after application of the nulling phase distribution can now be calculated and compared.
The objective of nulling is to improve signal quality by targeting a detrimental Nth order intermodulation beam and degrading the directivity of that beam such that either or both of the degradations (D1IB-D1IA) and (D2IB-D2IA) are large by comparison to corresponding fundamental beam degradations (D1FB-D1FA) and (D2FB-D2FA).
Simulations indicate in a 14×14 array with analog phase shifters PNi1, PNi2 the directivity of any odd-order intermodulation beam can be degraded by about 35 dB at a cost of fundamental beam degradation of less than 0.25 dB. Notably, using present day technology, digital phase shifter performance can be expected to fall short of that of analog devices owing to introduction of analog/digital conversion quantization errors.
In some embodiments, a collection of directivity patterns P are stored in a memory device such as a semiconductor or disc drive memory device. The value of P is the directivity of a particular beam. In some embodiments, the memory device 359 is a part of the intermodulation beam nulling computer 361 and in some embodiments the memory device 356 is a part of the beam forming section 350.
Pre-calculation and storage of directivity patterns avoids the need to calculate directivities after angle commands (θ0, φ0), (θ′0, φ′0) are given. Among other things, pre-calculation and storage saves time and reduces processor requirements. Notably, where commanded angles differ from stored angles, a selection methodology is required such as selection of the closest stored angle data and/or interpolation of the stored angle data to fit the commanded angles.
As persons of ordinary skill in the art will appreciate, stored directivity patterns P can be referenced in different ways. For example, the stored patterns can be stored in a multidimensional matrix such that
P=P(j,k,θ0p,φ0p,θ′0q,φ′0q,θ,φ)
where
1) j is an integer indicating the first fundamental beam (j=1), the second fundamental beam (j=2), the first 3rd order IM beam (j=3), the second 3rd order IM beam (j=4), the first 5th order IM beam (j=4), the second 5th order IM beam (j=5), and so on.
2) k is an integer indicating when nulling is applied (k=1) and when nulling is not applied (k=2).
3) θ0p, φ0p indicate the stored elevation and azimuth angles that are closest to the commanded angles for the first signal θ0, φ0.
4) θ′0p, φ0q indicate the stored elevation an azimuth angles that are closest to the commanded angles for the second signal θ′0, ′φ0.
5) and, where θ, φ indicate angles relative to the antenna platform's look angle, for example a spacecraft's look angle toward the earth. Here, the antenna pattern P will vary with θ, φ, such that for example, the peak of the first fundamental pattern occurs at angles θ0 and φ0.
In some embodiments, adaptation utilizing radiator feedback updates pattern values P to account for radiator element 320 changes such as radiator degradation.
Radiator degradation modifies the radiator's complex excitation coefficient Imn. As shown above, a radiator's modified excitation coefficient changes values of directivity D that were earlier stored as pattern values P. In essence, actual pattern values change as radiators degrade and stored pattern values are updated to maintain the performance of the nulling system.
a) the first attenuation block 622 applies attenuations A11, A12, A21, A22 . . . AM1, AM2 to equalize radiator amplitudes and
b) the nulling phase shifter block 624 applies phase shifts such that βi1=−βi2 for i=1 to M to null beams where β11=−β21=β31=−β41= . . . =90° /N
Sampling block 628 follows the nulling phase shifter block 624 and samples the forward and reflected traveling wave signal levels at the input of each antenna radiator as discussed above. The sampling block is coupled 608 to the pattern update decision block 600C.
If performance is not improved by applying a checkerboard nulling phase distribution, flow passes from decision block 620 to attenuation block 626 where a uniform attenuation and phase distribution is applied to the signals where A11=A21= . . . =AM1=A12=A22= . . . =AM2=0 and β11=β21= . . . =βM1=β12=β22= . . . =βM2=0.
If there is no significant change, then the process 600A is ready to accept another set of commanded angles 610. If there is a significant change, control passes to the pattern update process 642 which updates the antenna directivity patterns in read/write memory 359 containing fundamental and intermodulation antenna patterns using the directivity equation D and the new signal levels P(j, k, θ0p, φ0p, θ′0q, φ′0q, θ, φ).
After pattern updating is completed, the process 600A is ready to accept another set of commanded angles 610.
While various embodiments of the present invention have been described above, it should be understood that they have been presented by way of example only, and not limitation. It will be apparent to those skilled in the art that various changes in the form and details can be made without departing from the spirit and scope of the invention. As such, the breadth and scope of the present invention should not be limited by the above-described exemplary embodiments, but should be defined only in accordance with the following claims and equivalents thereof.
This invention was made with government support under Contract No. FA8802-04-C-0001 awarded by the Department of the Air Force. The government has certain rights in the invention.