[0001] The invention relates to a phase shift control for a phased array antenna, whereby
the antenna modules comprising the phase shifters are arranged in rows and columns,
which phase shift control is provided with computing means for caLcuLating the desired
phase setting for the separate phase shifters from at Least the beam direction to
be determined, the frequency of the energy emitted, and the position of each phase
shifter in the array.
[0002] Such a phase-shift control is known from, for example, M.I. Skolnik, "Introduction
to Radar Systems", 2
nd ed., McGraw-Hill Kogakusha, Ltd., 1980, p. 323, where the phase shift for the respective
antenna modules is determined in a beam-steering computer. If these phase shifts must
be determined for each radar pulse emitted, an exceptionally Large computer capacity
will be required for the usually Large number of antenna modules. This capacity can
be Limited by refraining from a phase setting per pulse and enabling this setting
after each transmission of a given pulse series or by performing the phase setting
in accordance with certain patterns. The present invention has for its object to provide
such a phase-shift control that with a strongly reduced computer capacity still a
phase setting per pulse and per antenna module can be achieved.
[0003] According to the invention, the computing means thereto comprises central computing
means for calculating, from the beam direction to be determined and the frequency
of the energy emitted, the terms in the mathematical expression for the phase setting,
which terms are the same for all phase shifters, and a computing chip present in each
antenna module for determining the desired phase setting from the terms determined
by the central computing means and the position of the separate phase shifters in
the array. The complete computer processes to be performed are therefore split into
processes performed centrally and processes performed locally, i.e. on antenna-module
LeveL.
[0004] If in a Cartesian coordinate system the x- and y-axes determine the antenna plane
and the z-axis the antenna main axis and it is assumed that the beam direction makes
an angle 0 with the z-axis and that the projection of the beam direction on the x-y
plane makes an angle ϕ with the x-axis, then for phase differences ψ and ψ
y between the phase shifters adjoining the x- and y-directions:


where d
1 is the distance between two antenna modules in the x-direction and d
2 the distance between two antenna modules in the y-direction. If all antenna modules
in the x-y plane are arranged above and next to each other, then for the phase shift
for antenna module m,n:

[0005] If on the other hand the rows of antenna modules are shifted alternately a distance
of ½d
1 in the x-direction with respect to each other, this phase shift wiLL be:

while maintaining the row and column configuration in the array. For simplicity, the
first situation in the array wiLL be considered here, so that

[0006] In the case of using a space-fed phased array antenna, either a Lens array or a reflect
array, a correction must be made in the expression for ψ
m,n. This correction allows for the change from a spherical to a plane phase front. To
this effect, the term

C
m,n is included in the expression for ψ
m,n . For the change from a purely snherical to a plane chase front.

where p is the distance between the centre of the horn radiator or other radiating
element and the antenna plane. Such a purely spherical phase front is not present
in practice. Since the C
m,n values are found to be frequency-dependent and no mathematical relationship between
C
m,n and the frequency can be indicated, C
m,n values for different frequency intervals must be established emperically.
[0007] During scanning with the antenna beam at certain elevations it is sometimes desirable
to widen the beam. This requires the introduction of an additional phase shift ε
m,n; consequently, no plane phase front is formed, but say a quadratic phase front.
[0008] For phase shift ψ
m,n the relationship is now:

where B=0 if no beam widening is applied; if applied, B=1. K is a constant. It is
known to calculate this phase shift for each antena module separately in a beam-steering
computer. According to the invention, the caLcuLation is however split into processes
performed centrally and processes performed LocaLLy in each antenna module. In the
case of centraLLy performed processes, the results can be fed to all antenna modules
simultaneously.
[0009] The terms

.cosϕ.sinθ,

.sinϕ.sinθ and c = X can be calculated centrally. Entry of the values d=m, e=n, f=C
m,n and g=ε
m,n into the computing chip of each antenna module is done once only, Leaving in each
chip only the calculation of

The d, e, f and g values can be stored permanently in each computing chip; they can
however also be supplied by the central computing means each time before the array
is activated. In such a case, the B-vaLue can be supplied as well; it is also possible
to enter this value separately or simultaneously with the a, b and c values when the
array is in the active mode.
[0010] The division between centrally and LocaLLy performed processes may be effected other
than described above. For instance,

the values a = cosϕ.sinθ, b = sinϕ.sinθ and can be determined centraLLy and, after
entry of the values d
= K.m.d
1,
e = K.n.d
2,
f = K.C
m,n and g = ε
m,n in the respective computing chips, the phase shift ψ
m,n = c.{a.d + b.e + f} + B.g locally, or the values

cosϕ.sinθ,

sinϕ.sinθ and

centraLLy, and after entry of the values d = K.m.d
1, e = K.n.d
2, f = K.C
m,n and g
= ε
m,n into the computing chips, the phase shift ψ
m,n = a.d + b.e + c.f + B.g LocaLLy.
[0011] The invention wiLL now be described with reference to the accompanying figure, showing
a block diagram of an embodiment of the phase-shift control in accordance with the
invention.
[0012] In this figure, the numeral 1 represents the central computing means. The computing
chip of each antenna module is designated by 2 and the associated phase shifter by
3. The antenna modules are thus formed by the elements 2 and 3 jointly. The data transmissions
from the central computing means 1 to the separate antenna modules 2, 3 are routed
via the buffer elements 4 by means of the addressing circuit 5.
[0013] Reading of the values d
= m, e
= n, f
= C
m,n and
g = ε
m,n into the separate computing chips takes place before the array antenna assumes the
active mode. The d-values are the same for the antenna modules Lying in a column.
ALL buffer elements 4 are therefore fiLLed with a certain m-value from the central
computing means. The e-values are the same for the antenna modules Lying in a row.
To enter these values, aLL buffer elements 4 are filled with the same n-value from
the central computing means, namely m successive times with a new n-value. The f-
and g-values are different for each antenna module. To enter these values, the buffer
elements are fiLLed m successive times with a certain C or m,n ε
m,n value from the central computing means. In all cases, the addressing circuit 5 ensures
that this information is entered intothe antenna modules.
[0014] Since the C
m,n values are frequency-dependent, it is preferable to enter several of such values
in each antenna module to ensure that, whenthe array is in the active mode, an appropriate
C
m,n value is avaiLabLe for the LocaLLy performed caLcuLations with each frequency change.
[0015] With the array antenna in the active mode, the values

d
1.cosϕ.sinθ,

d
2.sinϕ.sinθ and

, supplied to the antenna modules each time, are the same for all antenna modules.
The buffer elements 4 are fiLLed successively with the same a-, b- or c-value from
the central computing means 1, while the addressing circuit 5 again ensures that this
information is entered into the respective antenna modules. During the transmission
of a radar pulse and the Listening to an echo the a-, b- and c-values for a subsequent
radar pulse are entered into the antenna modules. In the dead time before the transmission
of the next radar pulse, only a command signal is sent to all antenna modules simultaneously
in the same way as the a-, b- and c-values,whereupon the array switches to the newly
selected beam direction.
1. Phase-shift control for a phased array antenna, whereby the antenna modules comprising
the phase shifters are arranged in rows and columns, which phase shift control is
provided with computing means for calculating the desired phase setting for the separate
phase shifters from at Least the beam direction to be determined, the frequency of
the energy emitted, and the position of each phase shifter in the array, characterised
in that the computing means comprises central computing means for caLcuLating from
the beam direction to be determined and the frequency of the energy emitted, the terms
in the mathematical expression for the phase setting, which terms are the same for
all phase shifters, and a computing chip present in each antenna module for determining
the desired phase setting from the terms determined by the central computing means
and the position of the separate phase shifters in the array.
2. Phase-shift control as claimed in claim 1, whereby a space-fed phased array antenna
is applied, characterised in that frequency-dependent correction values, required
for the phase setting of the phase shifters individually and the change from a spherical
to a plane phase front, can be entered into each computing chip.
3. Phase-shift control as claimed in claim 1 or 2, characterised in that a correction
value, required for the phase setting of the phase shifters individually and the beamwidth
setting, can be entered into each computing chip.