Antennae With Linear Aperture

The present invention relates to antennae with linear aperture.

It is often useful, for example in the case of airborne radars that the equivalent point source, or phase centre, of such an antenna should be movable, for example, in order to eliminate fixed echoes.

It is on object of this invention to provide such an antenna in which the phase centre can be moved along a straight line.

According to the invention there is provided a method for linearly displacing the phase centre of an antenna having a linear radiating aperture, with respect to an original phase centre corresponding to a symmetrical illumination of said aperture, said method consisting in illuminating said aperture with a linear and variable dissymmetry with respect to said original phase centre.

For a better understanding of the invention and to show how the same may be carried into effect reference will be made to the drawings accompanying the following description in which:

FIG. 1 shows diagrammatically the linear aperture of an antenna in two positions;

FIG. 2 shows an antenna embodying the improvement according to the invention;

FIG. 3 shows an embodiment of the improvement according to the invention used in an antenna according to FIG. 2;

FIG. 4 is a diagram explaining the interest of the invention in the case of an airborne radar; and

FIG. 5 shows an example of the application of the improved antenna according to the invention.

The radiation diagram of an antenna is given by the Fourier transform of the illumination on the radiating aperture of the antenna. For a linear aperture, such as AB in FIG. 1, and the centre point O of AB being selected as origin, a symmetrical illumination results in a radiation diagram which is equiphasal and symmetrical in modulus relative to the median plane of the aperture AB. The trace of this plane on that of the drawing is the straight line ON.

The phase centre of the antenna is at O.

If the aperture of the antenna is displayed by an amount d to A' B', the phase difference between the waves received at O and O' is: ##EQU1## WHERE .theta. IS THE ANGLE FORMED BY THE DIRECTION D of origin of the waves received, with ON, and .lambda. is the wave length.

If the illumination of the aperture is rendered non-symmetrical, the aperture being in the position AB, the radiation diagram of the antenna remains symmetrical in modulus, but becomes uneven in phase, that is to say, with O as origin, the function representing the phase as a function of the angle .theta. is odd.

For relatively small angles, it is possible without displacing the aperture AB to obtain, by a dissymmetry of illumination, a radiation having the same phase law at O', at a distance d from O as if the aperture AB had been moved by d. A wave coming from the direction .theta. and received by the antenna with unsymmetrical illumination of the radiating aperture is therefore equivalent, from the point of view of phase, to a wave received from the same direction by the antenna with symmetrical illumination displaced by d. Thus, by introducing a dissymmetry into the illumination of the aperture of the antenna according to the invention, the centre of the phase of the antenna is shifted along its aperture.

FIG. 2 shows an antenna of the pill box type, using the invention. It is, in fact, easy to change the illumination of a focusing system (paraboloidal cylinder, lens, etc.) by using, for example, a primary source consisting of several horns which may be phase shifted in a variable manner, one relative to the other.

FIG. 2 shows an antenna 1 of the pill box type, folded in order to eliminate the shadow of the primary source.

This antenna 1 comprises a double primary source 2 supplied by a wave guide 3. This source radiates in the direction of a reflector 4 in the form of a parabolic cylinder which transmits the energy supplied by the source towards the radiating aperture 5.

FIG. 3 shows diagrammatically an embodiment of the primary source 2.

The energy received from the guide 3 is divided amongst two channels 21 and 22 by means of a folded magic Tee 20, the fourth channel of which terminates in a matched load. The channels 21 and 22 comprise, respectively, phase shifters 23 and 24, for example, varactors. The phase-shift between the two channels is therefore variable by electric means. The energy passing through each of the two channels 21 and 22 is radiated respectively by the mouths 25 and 26. The phase-shift between the two channels shifts the illumination maximum of the reflector 4, and creates thereby the dissymmetry in the illumination of the radiating aperture AB. The phase centre of the antenna 1 is therefore mobile along AB as a function of the phase-shift between the two channels.

Such an antenna may, more particularly, be used in airborne radars for compensating at the reception the phase variation between two successive pulses, when the transmission of these impulses is coherent.

In FIG. 4, the axis O.sub.1 O.sub.2 x represents the flight line of the aircraft carrying the radar. Between two pulses, the aircraft has travelled a distance d, which represents the distance between the two positions O.sub.1 and O.sub.2 of the centre of the aperture of the antenna. If the transmission is effected with the same phase in the direction D of a fixed target, the direction D is determined by the angle .theta., and the echoes received for two successive pulses present a phase-shift 4 .pi. d/.lambda. sin .theta.. If, with the antenna according to the invention, the centre of the phase is shifted forwards at the first reception by an amount d (so that the phase centre coincides with O.sub.2), and backwards at the second reception (so that it coincides with O.sub.1), the dephasing between the echos received for the two successive impulses is compensated. To a coherent transmission corresponds a coherent reception.

It is also possible to utilize the shift of the phase centre both for the transmission and for the reception. In this case it is sufficient to displace the phase centre of the antenna by the amount d/2, in the forward direction during the transmission and the reception of the first pulse, and in the backward direction during the transmission and reception of the second pulse.

In this case, the phase centre of the antenna remains fixed and is located in the centre of O.sub.1 O.sub.2.

FIG. 5 shows an example of an application to an airborne radar in the case, where the phase centre is shifted only during the reception.

During the transmission, coherent pulses supplied by the transmitter 30 are transmitted without phase-shift to two apertures 25 and 26 by means of circulators 28 and 29.

During the reception, the echoes received from a target through the apertures 25 and 26 are passed to the receiver 31 via phase shifters 23 and 24.

These phase-shifters receive respectively the outputs 320 and 321 of a control voltage generator 32 which can have one or the other of two values in response to signals coming from the generator 33, generating the radar sync. signals. The operation of the system is a follows:

The signal relating to a target is produced by means of two successive pulses, that is to say, for example, by means of a so-called odd rank impulse followed by a so-called even rank impulse.

During the transmission of an odd impulse, the synchronizing signal generator 33 sends an impulse to the generator 32 which supplies at its outputs 320 and 321, respectively, the voltages V.sub.o + v and V.sub.o - v, wherein v is controlled in such a manner that the phase centre of the antenna is displaced by d in advance for the reception of the echo caused by this impulse. At the following even impulse, the voltages at the outputs 320 and 321 are reversed and the phase centre shifts therefore by the amount d in the backward direction for the reception of the echo (coming from the same target), caused by this even impulse. The voltage v is controlled according to the distance d desired, and especially as a function of the speed of the aircraft.

It may also be more practical in certain cases to keep constant the amplitude d of displacement of the phase centre. In this case, the absolute value of the relative phase-shift is maintained constant, and it is the pulse repetition frequency of the radar transmitter that is varied as a function of the speed of the aircraft.