[0001] Active phased array systems or smart antenna systems have the capability for performing
programmable changes in the complex gain (amplitude and phase) of the elemental signals
that are transmitted and/or received by each respective element of the phased array
system to accommodate different beam-forming scenarios. Communications satellites
equipped with phased array systems are desirable since satellites so equipped have
an intrinsic performance advantage over satellites with conventional reflector antennas.
For example, a communications satellite with a phased array system can offer the following
advantages: reconfigurable beam patterns ranging from broad-uniform continental coverage
down to narrow spot beam patterns with 3 dB widths of about 1°; flexibility in varying
the level of effective isotropic radiated power (EIRP) in multiple communication channels;
and means for providing graceful system performance degradation to compensate for
component failures. As conditions for the phased array system in the satellite can
change in an unpredictable manner, regularly scheduled calibration for characteristics
of the system, such as phase and amplitude characteristics, is generally required
to assure optimal system performance.
[0002] In order to obtain meaningful estimates of the respective complex gains for the elemental
signals respectively formed in each element of the phased array system, the calibration
process must be performed in a time window that is sufficiently short so that the
complex gains for the respective elemental signals transmitted from each element are
substantially quasi-stationary. For a typical geostationary satellite application,
the relevant time windows are dominated by two temporally variable effects: changes
in the transmitted elemental signals due to variable atmospheric conditions encountered
when such signals propagate toward a suitable control station located on Earth; and
changes in the relative phase of the transmitted elemental signals due to thermally
induced effects in the satellite, such as phase offsets in the respective circuit
components for each respective element of the phased array system, and physical warpage
of a panel structure employed for supporting the phased array. The thermally induced
effects are caused primarily by diurnal variations of the solar irradiance on the
phased array panel.
[0003] Calibration techniques proposed heretofore are essentially variations on the theme
of individually measuring, one at a time, the respective complex gain of each single
element (SE) of the phased array system while all the other elements of the phased
array system are turned off. Although these calibration techniques (herein referred
as SE calibration techniques) are conceptually simple, these SE calibration techniques
unfortunately have some fundamental problems that make their usefulness questionable
for meeting the calibration requirements of typical phased array systems for communications
satellites. One problem is the difficulty of implementing a multipole microwave switching
device coupled at the front end of the respective electrical paths for each elemental
signal so as to direct or route suitable test signals to any single element undergoing
calibration. This multipole switching device is typically necessary in the SE calibration
techniques to measure the complex gain for the elemental signal respectively formed
in any individual element undergoing calibration at any given time. Another problem
of the SE calibration techniques is their relatively low signal-to-noise ratio (SNR).
This effectively translates into relatively long measurement integration times. At
practical satellite power levels, the integration times required to extract the calibration
measurements for the SE calibration techniques are often too long to satisfy the quasi-stationarity
time window criteria described above. In principle, one could increase the effective
SNR of the SE process by increasing the power of the calibration signals transmitted
from each element. However, as each element of the phased array system is usually
designed to operate at near maximum power, as dictated by the power-handling capacity
and linearity constraints for the circuit components in each element, it follows that
arbitrary additional increases in power levels are typically not feasible. Thus it
is desirable to provide a calibration method that allows for overcoming the problems
associated with SE calibration techniques.
[0004] Generally speaking, the present invention fulfills the foregoing needs by providing
a method and apparatus for remotely calibrating a system having a plurality of N elements,
N being a positive integer number. The method includes generating coherent signals,
such as a calibration signal and a reference signal having a predetermined spectral
relationship between one another. The calibration signal which is applied to each
respective one of the plurality of N elements can be orthogonally encoded based on
the entries of a predetermined invertible encoding matrix, such as a binary Hadamard
matrix, to generate first and second sets of orthogonally encoded signals. The first
and second sets of encoded signals and the reference signal are transmitted to a remote
location. The transmitted first and second sets of encoded signals are coherently
detected at the remote location. The coherently detected first and second sets of
encoded signals are then decoded using the inverse of the predetermined invertible
encoding matrix to generate a set of decoded signals. The set of decoded signals is
then processed for generating calibration data for each element of the system.
[0005] The invention may best be understood by reference to the following detailed description
in conjunction with the accompanying drawings in which like numerals represent like
parts throughout the drawings, and in which:
Fig. 1 is a simplified block diagram representation of a communications satellite
using a phased array system that can be remotely calibrated in accordance with the
present invention from a remote control station;
Fig. 2 is a block diagram representation showing an exemplary architecture for the
phased array system of Fig. 1, and including a coherent signal generator and a controller
for controllably switching respective delay circuits in each element of the phased
array system in accordance with one embodiment for the present invention;
Figs. 3a and 3b illustrate, respectively, gain characteristics for a single delay
circuit being switched-in, and for multiple (two) delay circuits being switched-in
in any given one of the elements of the phased array system of Fig. 2;
Fig. 4 shows further details about the coherent signal generator of Fig. 2;
Fig. 5 is a simplified block diagram for a coherent detector and a calibration processor
situated at the remote control station of Fig. 1;
Fig. 6 shows further details about the coherent detector of Fig. 5;
Fig. 7 is a flowchart of an exemplary embodiment for a calibration method in accordance
with the present invention;
Fig. 8 is a flowchart showing steps used for orthogonally encoding signals in a coherent
system, such as the phased array system of Fig. 2;
Fig. 9 is a flowchart showing steps used for measuring in-phase and quadrature components
of orthogonally encoded signals and for decoding the measured in-phase and quadrature
components of the orthogonally encoded signals; and
Fig. 10 is a flowchart showing steps for sequentially transmitting the orthogonally
encoded signals used for calibrating the phased array system of Fig. 2.
[0006] Figure 1 illustrates a communications satellite 10 that incorporates a phased array
system 12 for transmitting and/or receiving radio frequency (RF) signals 14. If, for
example, phased array system 12 is used in a transmitting mode, then RF signals 14
can be received at a remote control station 18, such as an earth-based control station,
through a receiving antenna 20. As will be appreciated by those skilled in the art,
a phased array system operates on the principle that the phase of the RF signals emitted
from the elements of the array can be selectively adjusted to provide a desired interference
pattern at locations that are spatially remote from each element of the phased array.
Consider an RF transmission from an N-element phased array system at wavelength λ.
By way of example, choose a coordinate system with its origin at the center of the
phased array. The signals A(
i), received at spatial points
i, are the interference sum of N elemental signals,

having waveforms s(n,
i), such that

[0007] The relative values of the set of coefficients, {a(n)}, give the relative complex
gains associated with respective circuit components, such as phase shifters 50 (Fig.
2) and power amplifiers 80 (Fig. 2), for each element of the phased array. It can
be shown that information merely obtained by spatially sampling any interference pattern
transmitted and/or received by the phased array (but not encoded in accordance with
the present invention) cannot easily extract phase offsets due to the relative positioning
of the elemental horns of the phased array, such as transmitting horns 90 (Fig. 2).
In principle, the value for each coefficient a(n) could be determined by measuring
or sampling the amplitude and phase of the interference pattern at N distinct spatial
sampling locations {
i}; i= 1, 2, ..., N, that are specifically selected to provide N linearly independent
simultaneous equations. In practice this procedure would be very difficult to implement
as N values of three different parameters would have to be known to compute a solution.
The three different parameters include the spatial sampling {
i}, the elemental transmitting horn positions
n, and the relative values of the different propagation constants K
i.
[0008] In contrast to the above-described spatial sampling calibration technique, coherent
signal encoding of the elemental signals provides a dramatic simplification as the
encoded signals, which enable to form predetermined time multiplexed beam patterns,
can be received at a single receiver point situated along a reference direction
0. Further, as there is only one propagation constant K
0, its value need not be known to determine the respective relative values of each
complex gain. Also, in the far field, the parameters of interest can be obtained without
knowledge of the distance to the single receiver point. It is assumed that the projection
angle of reference direction
0 onto the uniform phase plane of the array is known to a precision commensurate with
the desired calibration accuracy. As will be appreciated by those skilled in the art,
the projection angle can be measured using readily available attitude measurements
from conventional celestial body sensors, such as Earth, Moon and Sun sensors.
[0009] In the far field, the received signal of any mth coherently encoded transmission
is of the form,

for m = 1, 2, ..., N.
[0010] If t(m,n) represents the coefficients of a predetermined invertible, encoding matrix
T, such as an unitary, encoding matrix, then the respective relative values of the
product

can be obtained directly from the inversion of matrix
T which enables for solving a system of N linearly independent simultaneous equations.
In general, the inverse of a unitary matrix
U is equal to the Hermitian conjugate
U* of the matrix
U and thus
U-1 ≡
U*. As will be appreciated by those skilled in the art, the rows and columns of a unitary
matrix, such as matrix
U, form a complete orthonormal set of basis vectors that span the vector space upon
which matrix
U is defined. In general, orthogonal transforms are formally defined as the subset
of unitary transformations defined on real vector spaces. Orthogonal transforms have
been used extensively in imaging applications; see, for example, technical paper by
W. K. Pratt, J. Kane, and H. C. Andrews, "Hadamard Transform Image Coding", Proc.
IEEE 57, No. 1, at 58-68, (January 1969). As used herein the matrix
T differs from its associated unitary matrix by a normalization factor

. Accordingly,
T is referred as a renormalized unitary matrix,

[0011] By way of example and not of limitation, it can be shown that a minimum variance
encoding scheme can be achieved when using a renormalized unitary matrix where each
matrix element has unit magnitude, i.e.,

= 1. Some notable examples of equal magnitude renormalized unitary matrices are the
classes of two-dimensional (2D) discrete Fourier transforms (DFT) and Hadamard matrices.
[0012] Fig. 2 shows a simplified schematic of an exemplary analog architecture for an N-element
phased array system 12. It will be appreciated that the present invention need not
be limited to analog architectures being that digital beam-forming architectures can
readily benefit from the teachings of the present invention. It will be further appreciated
that the present invention need not be limited to a phased array system being that
any system that employs coherent signals, such as coherent electromagnetic signals
employed in radar, lidar, communications systems and the like; or coherent sound signals
employed in sonar, ultrasound systems and the like, can readily benefit from the teachings
of the present invention.
[0013] Phased array system 12 includes a beam-forming matrix 40 made up of N phase shifters
50
1 - 50
N each having a p-bit beamforming capability. Each respective phase shifter for each
element is made up of p independent delay circuits 60 that, by way of suitable switches
65, can be selectively switched or actuated into the electrical path for each elemental
signal to provide 2
p quantized phase levels corresponding to phase shifts of 2πm/2
P for m = 0, 1, ..., 2
P-1. Fig. 2 further shows a coherent signal generator 100 that supplies a reference
tone or signal having a predetermined spectral relationship with respect to a calibration
signal applied to each element of the phased array. For example, the reference signal
can be offset in frequency by a predetermined factor from the calibration signal.
The reference signal and the calibration signal each passes through respective bandpass
filters 72 having a predetermined passband substantially centered about the respective
frequencies for the reference signal and the calibration signal. Although in Fig.
2 coherent signal generator 100 is shown as supplying one reference signal, it will
be appreciated that additional reference signals, if desired, could be readily obtained
from coherent signal generator 100.
[0014] As shown in Fig. 2, each phased array element further includes a respective power
amplifier 80 and a respective horn 90. Although Fig. 2 shows that the reference signal
is transmitted from a separate horn 90', the reference signal can, with equivalent
results, be transmitted from any of the phased array elements as long as the reference
signal is injected into the electrical path after any of the phase shifters 50
1 - 50
N so that the reference signal is unaffected by any encoding procedures performed by
the phase shifters. Fig. 2 shows a controller 300 which, during normal operation of
the system, can issue switching commands for forming any desired beam patterns.
[0015] In accordance with one preferred embodiment for the present invention, controller
300 further includes a calibration commands module 302 for issuing first and second
sets of switching signals that allow the delay circuits 60 for encoding corresponding
first and second sets of signals being transmitted by the N elements of the phased
array system to a remote location, such as control station 18 (Fig. 1).
[0016] As suggested above, the controlled switching, i.e., the encoding, is dictated by
the matrix elements or entries of a predetermined invertible, binary matrix. In particular,
a class of orthogonal matrices, such as binary or bipolar Hadamard matrices, is optimal
in the sense of providing minimal statistical variance for the estimated calibration
parameters. The encoding matrix can be chosen to have a size NxN if N is an even number
for which a Hadamard matrix can be constructed. If a Hadamard matrix of order N cannot
be constructed, then the next higher order Hadamard construction can be conveniently
used for the encoding. For example, the next higher order can be conveniently chosen
as K=N+Q where Q is a positive integer number representing extra transmissions corresponding
to non-existing elements and thus such extra transmissions are effectively treated
as if they were made up of zero value signals. It will be appreciated by those skilled
in the art that this matrix construction technique is analogous to "zero-filling"
techniques used in a Fast Fourier transform, for example. Henceforth in our discussion
for the sake of simplicity and not by way of limitation we will only consider Hadamard
matrices, represented by
H for the controlled switching (CS) procedure. It will be shown that upon performing
suitable coherent detection and decoding at the remote location, the first and second
sets of orthogonally encoded signals allow for determining calibration data indicative
of any changes in the respective complex gains of the delay circuits, and including
the respective signals {s(n) for n= 1, 2, ..., N} associated with each of the phased
array elements when no delay circuit is switched-in, i.e., each signal associated
with a respective undelayed or "straight-through" electrical path that includes the
respective power amplifier and horn but does not include any delay circuit in any
respective phased array element.
[0017] For an analog embodiment, it is assumed that the power levels for the calibration
signal are low enough so that the phase shifters can be treated as linear microwave
devices. For example, the effect of switching-in or actuating a single delay circuit
60, such as the µth delay circuit in any nth phase shifter with a complex gain d
µ(n) simply imposes a complex gain as shown in Fig. 3a to an input signal x(n). The
effect of switching-in or actuating multiple delay circuits 60 and 60' simply generates
the product of the respective complex gains for the multiple circuits switched-in.
For example, as shown in Fig. 3b, if the νth delay circuit for the nth phase shifter
with a complex gain d
ν(n) is switched-in together with the µth delay circuit, then the complex gain for
the input signal x(n) will be as shown in Fig. 3b.
[0018] Fig. 4 shows a simplified schematic for coherent signal generator 100 used for generating
coherent signals, such as the calibration signal and the reference signal. As used
herein the expression coherent signals refers to signals having a substantially constant
relative phase relation between one another. As shown in Fig. 4, a local oscillator
102 supplies an oscillator output signal having a predetermined frequency f
o to respective frequency multipliers 104, 106 and 108 each respectively multiplying
the frequency of the oscillator output signal by a respective multiplying factor such
as N
1, N
2 and N
3, respectively. As shown in Fig. 4, the respective output signals of multipliers 108
and 104 is mixed in a first mixer 110 to supply a first mixer output signal having
a frequency f=(N
2+N
3)f
o. Similarly, the respective output signals of multipliers 106 and 108 are mixed in
a second mixer 112 to supply a second mixer output signal having a frequency f=(N
1+N
3)f
o. By way of example, the first mixer output signal can constitute the reference signal
and the second mixer output signal can constitute the calibrated signal applied to
each element of the phased array system.
[0019] Fig. 5 shows a simplified block diagram for a coherent detector 400 and a calibration
processor 402 which can be situated at control station 18 (Fig. 1) for detecting and
decoding, respectively, any sequences of encoded coherent signals being transmitted
from the phased array system for determining calibration data which can then be conveniently
"uplinked" to the satellite to compensate for changes in the various components which
make up each respective element of the phased array system, such as power amplifiers,
horns, and phase shifters.
[0020] Fig. 6 shows details about coherent detector 400 and calibration processor 402. As
shown in Fig. 6, the received reference signal is supplied to a first mixer 406 and
to a phase shifter 404, which imparts a phase shift of substantially 90° to the received
coherent reference signal. As further shown in Fig. 6, each orthogonally encoded signal
is supplied to first and second mixers 406 and 408, respectively. First mixer 406
mixes any received encoded signal with the reference signal to supply a first mixer
output signal replicating the respective component of any received encoded signal
that is in phase with the reference signal. Conversely, second mixer 408 mixes any
received encoded signal with the phase shifted reference signal to supply a second
mixer output signal replicating the respective component of any received encoded signal
that is in quadrature (at 90°) with the reference signal. The in-phase and quadrature
components are converted to digital data by respective analog-to-digital (A/D) converters
409. As shown in Fig. 6, calibration processor 402 can include register arrays 410
1 and 410
2 for storing, respectively, the in-phase components and the quadrature components
supplied by A/D converters 409. Calibration processor 402 can further include a memory
412 that can store entries for the inverse matrix
H-1 which is used for decoding the respective quadrature components of the encoded signals.
Calibration processor 402 further includes an arithmetic logic unit (ALU) 412 for
performing any suitable computations used for decoding the respective quadrature components
of the encoded signals. For example, ALU 412 can be used for computing a difference
between each quadrature component for the first and second sets of orthogonally encoded
signal, and computing the product of the resulting difference with the inverse matrix
H-1,.
[0021] Fig. 7 shows a flow chart for an exemplary calibration method in accordance with
the present invention. After start of operations in step 200, step 204 allows for
generating coherent signals, such as the calibration signal and reference signal generated
by coherent signal generator 100 (Figs 2 and 4). In accordance with step 204, the
calibration signal is applied to each element of an N-element coherent system, such
as the phased array system of Fig. 2. Step 206 allows for encoding the calibration
signal applied to each element of the coherent system to generate, for example, first
and second sets of encoded signals. The encoding can be advantageously performed using
controlled switching or toggling of the delay circuits in each element of the phased
array system, that is, no additional or separate encoding hardware is required being
that the encoding is performed based on the specific delay circuits that are actuated
in response to the switching signals from calibration commands module 110 (Fig. 2).
For another preferred embodiment which uses a unitary transform encoder for orthogonally
encoding the calibration signal applied to each element of the phased array system,
the reader is referred to our US patent application Serial No. 08/499,796 (RD-24,492),
from which the present application claims priority.
[0022] Step 208 allows for transmitting the first and second sets of encoded signals and
the reference signal to a remote location, such as control station 18 (Fig 1). Step
210 allows for coherently detecting the transmitted first and second sets of encoded
signals at the remote location. Step 212 allows for decoding the detected first and
second sets of encoded signals to generate a set of decoded signals which can be conveniently
processed in step 214, prior to end of operations in step 216, for generating calibration
data for each element of the phased array system.
[0023] Fig. 8 shows a flow chart, which can be conveniently used for performing encoding
step 206 (Fig. 7) in the phased array system of Fig. 2. After start of operations
in step 222, step 224 allows for generating a first set of switching signals based
upon entries of invertible, binary matrix
H. Step 226 allows for applying the first set of switching signals to actuate respective
ones of the p delay circuits in each element of the phased array system to generate
the first set of encoded signals. In contrast, as shown in step 228, the second set
of switching signals uses -
H for the controlled switching which in turn generates the second set of encoded signals.
Prior to end of operations in step 232, step 230 allows for applying the second set
of switching signals to actuate respective ones of the p delay circuits in each element
of the phased array to generate the second set of encoded signals. This switching
procedure using a Hadamard control matrix effectively generates an exact unitary (orthogonal)
transform encoding of the calibration signal applied to each of the phased array elements.
As suggested above, this switching scheme is particularly advantageous being that
the delay circuits themselves provide the desired encoding, and thus no additional
encoding hardware is required.
[0024] Fig. 9 shows a flowchart that can be used for performing, respectively, detecting
step 210 and decoding step 212 (Fig. 7). After start of operations in step 240, and
assuming that the first and second sets of encoded signals are made up, respectively,
of first and second sets of orthogonally encoded signals, step 242 allows for measuring,
with respect to the reference signal, respective in-phase and quadrature components
for the first and second sets of orthogonally encoded signals which are received at
the remote location. For example, coherent detector 400 (Fig. 6) allows for measuring
both in-phase components and quadrature components of any received encoded signals.
This can further include measuring, with respect to the reference signal, the phase
and amplitude for each first and second sets of orthogonally encoded signals which
are received at the remote location. It will be appreciated that absolute measurements
are not important since the calibration data can be effectively obtained from relative
measurements of phase and amplitude, i.e., respective measurements of variation over
time of phase and amplitude for each received encoded signal relative to the phase
of the reference signal. Step 244 allows for computing a respective difference between
each respective measured in-phase and quadrature components for the first and second
sets of orthogonally encoded signals which are received at the remote location. Prior
to end of operations in step 248, step 246 allows for computing the product of each
respective computed difference with the inverse of the same binary orthogonal matrix,
H-1 =
HT/N used in the controlled switching encoding. In accordance with another advantage
of the present invention, it will be appreciated that the computation of inverse matrix
H-1 is straightforward since the inverse matrix in this case is simply the transpose
of
H normalized by the factor 1/N.
[0025] Fig. 10 shows a flowchart which provides further details about transmitting step
208 (Fig. 7) which allows for calibrating the full set of N(p+1) state variables associated
with, for example, the N elements for the phased array system of Fig. 2. It will be
shown that the controlled switching calibration procedure in accordance with the present
invention generally requires a total of 2N(p+2) individual sequential transmissions,
or N(p+2) sequential transmission pairs, that is, sequentially transmitting N(p+2)
pairs of the first and second sets of orthogonally encoded signals. This advantageously
enables the calibration procedure in accordance with the present invention to provide
information comparable to a SE calibration measurement at a signal-to-noise ratio
(SNR) effectively enhanced by a factor

2N over the SE calibration measurement with the same maximum elemental signal power
for each transmission.
[0026] After start of operations in step 260, step 262 allows for sequentially transmitting
N pairs of orthogonally encoded signals, such as corresponding to the first and second
sets of orthogonally encoded signals, wherein each µth delay circuit is switched in
accordance with predetermined encoding rules based upon entries of matrix
H, while each remaining delay circuit in each element of the phased array system is
switched-out. Each sequentially received transmission pair is conveniently expressed
in vector form as,

[0027] The first subscript index µ on ψ
µ0 indicates that a predetermined delay circuit, such as the µth delay circuit, is toggled
in accordance with predetermined encoding rules based upon entries of Hadamard matrix
H. The second subscript (zero) on these vector signals indicates that these are the
signals received when each remaining delay circuit, other than the µth delay circuit,
is switched-out. For this step of the calibration process, N transmission pairs of
orthogonally encoded signals corresponding to the N elements of the phased array system
are sequentially transmitted and received at the remote location.
[0028] Any mth sequentially received transmission pair of the first and second sets of orthogonally
encoded signals is, respectively, represented by,

[0029] The encoding coefficients D
µ(mn), D

(mn) are dictated by the status of the delay circuits that are switched according
to the following Hadamard encoding rules:


[0030] The differences of the encoding matrices are represented in component and matrix
form as,

[0031] As suggested above, decoding can be conveniently performed at the remote location
by computing the difference of received signal vectors ψ
µ0, ψ
Rµ0 and multiplying the resulting vector difference by the inverse of the same Hadamard
matrix that was used in the controlled switching performed onboard the satellite.
In the absence of noise, we obtain a decoded vector signal
Zµ0, such that,

[0032] Step 264 allows for transmitting N(p-1) pairs of orthogonally encoded signals wherein
each µth delay circuit is toggled in accordance with the predetermined encoding rules
while another predetermined delay circuit other than the µth delay circuit, say the
νth delay circuit, is permanently switched-in on each of the elements of the phased
array. In this case, any mth received transmission pair of the first and second sets
of orthogonally encoded signals is represented, respectively, by

[0033] Here again, the first subscript index µ on any component y
µν indicates that the µth delay circuit is toggled in accordance with the predetermined
encoding rules based upon entries of the predetermined Hadamard matrix
H while the second subscript index (here the ν index) indicates that the νth delay
circuit is switched-in on each of the elements of the phased array system. In this
case the resulting set of decoded signals are represented in vector form by a decoded
vector
Zµν , such that

[0034] The N complex gains, d
ν(n) are readily computed by taking the ratio of the decoded vector signal components,

[0035] The above-described procedure can be repeated using controlled switching with the
predetermined µth delay circuit and with each of the other remaining delay circuits
singly switched-in to determine each complex gain, d
ν(n) for all (p-1) remaining delay circuits such that ν ≠ µ. In this manner, step 264
allows for transmitting N(p-1) pairs of first and second sets of orthogonally encoded
signals wherein the predetermined µth delay circuit is toggled in accordance with
the predetermined encoding rules, while each remaining vth delay circuit in each phase-shifting
element of the phased array is sequentially switched-in.
[0036] Step 266 allows for transmitting N pairs of first and second sets of orthogonally
encoded signals wherein any delay circuit other than the µth delay circuit, for example
the ξth delay circuit (ξth ≠ µTH), is toggled in accordance with the predetermined
encoding rules, while each remaining delay circuit in each element of the phased array
system is switched out. In this case, the resulting set of decoded signals are represented
in vector form by decoded vector signal Z
ξ0, such that

[0037] Step 268 allows for transmitting N pairs of first and second sets of orthogonally
encoded signals wherein the ξth delay circuit is toggled in accordance with the predetermined
encoding rules, while the predetermined µth delay circuit in each phase shifter of
the phased array system is switched in. In this case the resulting set of decoded
signals are represented in vector form by decoded vector signal Z
ξµ such that

[0038] The N complex gains d
µ (n) are readily computed by taking the ratio of the decoded vector signal components,

[0039] Once all the respective complex gains d
γ(n) are determined for all γ = 1, 2,...,p; n = 1, 2,..., N, the "straight-through"
signals or undelayed signals, {s(n)}, are readily determined from,

[0040] Thus the complete calibration data for each respective complex gain for Nxp delay
circuits plus the complex gains for the N straight-through or undelayed electrical
paths are obtained with N(p+2) transmission pairs that can be conveniently enumerated
as follows:
[0041]

Mathematics of Hadamard Control Matrices
[0042] An Nth order Hadamard matrix 2 is an NxN binary orthogonal matrix with each entry,
[
H]
mn =
H(
mn) equal either to ± 1. An Nth order Hadamard matrix is not unique, as any permutation
of the rows or columns also produces an additional Nth order Hadamard matrix. Hadamard
matrices are orthogonal matrices with inverses,
H-1 =
HT/N. As an example, we illustrate the recursive generation of the set of radix 2 natural
form Hadamard matrices. Consider a fundamental matrix of order N=2.

[0043] An N=4th order natural form Hadamard matrix can be constructed as:

[0044] The "natural form" Hadamard matrix of order 2N can be constructed from the Nth order
Hadamard matrix using,

[0045] The orthogonal encoding using a Hadamard control matrix is based upon the following
procedure. Consider a diagonal matrix
d of complex numbers,
d ≡
diag[
d(1),
d(2), ...
d(
N)]. Construct matrices,
D,
DR, based upon any suitable Hadamard matrix with their (mn)th matrix elements or entries
constructed according to the following rules:

[0046] Matrices of the differences of
D,
DR are expressed in component and matrix form as,

[0047] Here
I is the identity matrix. Multiplying each side of Eq. (21) by the inverse matrix
H-1, gives a diagonal matrix,

[0048] While only certain features of the invention have been illustrated and described
herein, many modifications, substitutions, changes, and equivalents will now occur
to those skilled in the art. For example, although the above-described mathematical
background illustrates use of Hadamard matrixes in their "natural form", it will be
understood that the orthogonal encoding can be performed using all forms of Hadamard
matrixes and thus the present invention is not limited to "natural form" Hadamard
matrixes.
1. Apparatus for remotely calibrating a system having a plurality of N elements, N being
a positive integer number, said apparatus comprising:
a coherent signal generator for generating a calibration signal and a reference signal
having a predetermined spectral relationship between one another;
means for applying to each respective one of said plurality of N elements the calibration
signal;
means for encoding the calibration signal applied to each respective one of said plurality
of N elements to generate a set of encoded signals;
means for transmitting the set of encoded signals and the reference signal to a remote
location;
a coherent detector for detecting the transmitted set of encoded signals at the remote
location;
means for decoding the coherently detected set of encoded signals to generate a set
of decoded signals; and
a signal processor for processing the set of decoded signals for generating calibration
data for each element of said system.
2. The apparatus of claim 1, wherein said system comprises a phased array system.
3. The apparatus of claim 2, wherein each of said N elements in said phased array system
includes a plurality of p delay circuits.
4. The apparatus of claim 1, wherein each of said N elements in said phased array system
includes a plurality of p delay circuits, and wherein said means for encoding comprises:
means for generating a set of calibration switching signals based upon entries of
a predetermined invertible matrix H; and
means for applying the set of calibration switching signals to actuate respective
ones of the p delay circuits in each of the N elements so as to generate the first
set of encoded signals.
5. The apparatus of claim 4, wherein said invertible matrix H comprises a binary matrix
having at least a size NxN.
6. The apparatus of claim 4, wherein said means for encoding further comprises:
means for generating a second set of calibration switching signals based upon entries
of another invertible matrix defined by the product of (-1)H; and
means for applying the second set of calibration switching signals to actuate respective
ones of the p delay circuits in each of the N elements so as to generate the second
set of encoded signals.
7. The apparatus of claim 6, wherein said means for transmitting in operation transmits
a total of N(p+2) pairs of the first and second sets of orthogonally encoded signals.
8. The apparatus of claim 1, wherein the set of encoded signals generated by said means
for encoding comprises a set of orthogonally encoded signals, and wherein said coherent
detector comprises means for measuring, with respect to said reference signal, respective
in-phase and quadrature components for the set of orthogonally encoded signals being
received at the remote location.
9. The apparatus of claim 8, wherein said means for decoding comprises:
means for computing the product of each respective measured in-phase and quadrature
components with the inverse matrix T-1 of matrix T.
10. The apparatus of claim 8, wherein said means for measuring respective in-phase and
quadrature components for the set of orthogonally encoded signals comprises means
for measuring, with respect to said eference signal, phase and amplitude of the set
of orthogonally encoded signals being received at the remote location.