Antenna beamwidth and gain
Ships are designed specifically to detect targets, which are lying virtually in the horizontal plane. The antenna therefore propagates in a fan-shaped beam, narrow in the horizontal plane and relatively wide in the vertical plane.
Since the antenna has direction in a particular direction, it is said to have a power gain in that direction. Antenna gain is an important radar parameter and power gain in particular is considered in the radar equation.
Beamwidth is another of the important criteria since it specifies boundaries within the antenna radiation pattern, which are considered to be the limit of useful radiation (or reception).
Above shows the concept of beamwidth. This shows that because the beam shape of a radar antenna is not conical with the cone apex at the antenna, there exist two important beamwidth figures.
One is in the horizontal plane, known as the horizontal beamwidth (HBW) and the other is in the vertical plane, being known as the vertical beamwidth (VBW).
The HBW tends to assume more importance than the VBW because of its effect on the radar’s bearing discrimination.
The VBW however is large due to the fact that the target has to be hit by the beam even in a rough sea condition, when the ship is rolling. And also minimize unwanted echoes from the surface of the sea whilst optimizing the power gain characteristics of the antenna.
In the above it is seen a target which is struck by a portion of the Radar beam. The bold line shows the useful main lobe of the radiation. Power measured at A, B, C and D is one-half the measured power at the main lobe axis along which maximum radiated power acts. These (and other points lying on the ellipse ABCD), are known as the half-power points within the beam.
Beamwidth defined; the decibel; minor lobes
The horizontal or vertical beamwidth is then conveniently defined as the angle subtended by the selected half-power points at the antenna. The half-power points are also known as the minus three decibel points or three decibels down points, written -3dB and meaning 3 decibels lower than the maximum power measured at the main lobe axis at range R.
Vertical beamwidth (VBW) is generally between 22-25 degrees and horizontal beamwidth (HBW) generally between 0.8-1.5 degrees.
Note that the main transmitted lobe or major lobe does not contain all the transmitted power. Minor radiation lobes (side lobes) also exist, but the powers in those lobes are greatly reduced. Such a power reduction in normal circumstances causes no effect on echoes from a distant target. However sidelobes do cause secondary echoes, particularly from targets at short ranges. Slotted waveguide antennas minimize such lobes.
Relationships between HBW and VBW for slotted waveguide antennas are shown above. Also shown is the relative sidelobe power level relative to the main lobe axis at ± 10 degrees from that axis.
Antenna size HBW degrees VBW degrees Sidelobes± 10 degrees
12’ S band 1.85 22 -28 dB
12’ X band 0.65 22 -30 dB
9’ X band 0.85 22 -29 dB
Antenna aperture or effective area
Generally for a given wavelength, increasing the aperture will increase the power gain and decrease the horizontal beamwidth.
Azimuth bearing transmitter and receiver
It is a small machine driven via a gear train from the antenna drive unit. The machine is the electrical bearing transmitter.
The machines send to the display, the bearing information from the antenna to the display.
The antenna should be placed in a position that avoids or minimizes obstacles presented by the ship’s structure in the path of the radiated beam. Such obstacles produce shadow sectors and blind areas, which can hide targets of navigational importance and give rise to false echoes appearing on the PPI.
Antenna height above sea level is also of importance, since it has an effect on the radar horizon; in principle, radar range improves with height. A practical limit is reached when the incident angle of the vertical beam lobe extremities becomes sufficiently acute to return strong echoes from the sea surface which increases sea clutter at the display and can obscure targets at close range.
There is also a practical limitation placed on the amount length of the waveguide run.
The RF wave an effect known as diffraction by introducing slight differences in the velocity components at different parts of the wavefront.
Diffraction causes the path of the wave to follow the earth’s curvature for a distance determined by such factors as frequency, surface conductivity and atmospheric permittivity. The diffraction effect is greater for lower propagation frequencies and ten-centimetre wavelengths will bend to follow the earth’s surface for a greater distance than will three-centimetre wavelengths, other factors being equal
Very small targets close to the ship which might otherwise be easily discriminated may not adequately be irradiated by the main beam if the antenna height is too great; this and the increased sea clutter return can cause such target return to be lost on the display.
Aerial Rotation Rate:
As per the IMO performance standards the antenna should rotate at a constant speed of not less that 12 rpm in winds up to 100 knots.
Let us assume that an antenna rotates at a rate of 12 rpm –
Thus it rotates at 12 rotations in 60 seconds.
Or we can say that it does 1 rotation in 5 seconds.
Now if we have a Horizontal Beam Width (HBW) of 2°, then the time required to sweep through this 2° of HBW would take:
From the above:
1 rotation in 5 seconds
: 360° in 5 seconds
: 2° in (5/360) x2
And from this we can derive that the time required to sweep through the HBW (or any angle) would take:
T = HBW (or any angle) / 6 N where N is the rpm of the antenna, and T is the required time period.
Also the number of pulses striking a target of negligible width would be (theoretically) given by:
S = PRF x T where S is the number of pulses and T is the time period.
Combining the two we have:
S = PRF x (HBW/6N)
So if we have a PRF of 1000pps and a HBW of 2° and a scanner rotation speed of 12 rpm
Then the number of pulses that will theoretically strike a point target would be:
S = 1000 x (2 / 6x12)
= 1000 x (1/36)
= 28 pulses nearly
However in general at strike rate of 10 pulses is supposed to be great in sending back satisfactory number of echoes (some returning pulse would not be directed towards the scanner).
If this be so and if we assume that the HBW of a Radar set is at the limit of the IMO performance standard of 2.5° and the PRF is at 1000 pps, then the antenna rotation speed will be - using the above equation:
10 = 1000 x (2/6N)
Or N = 33.3 rpm
For the Heading Mark on a Radar, the IMO performance standard states that it should not be more than 0.5° thick. The heading mark should be displayed with an error of not greater than +/- 1°.
The Slotted Wave Guide Aerial:
From physics: If an alternating signal is applied across the mid length of a slot in a sheet of conducting material, then this slot would act as a effective radiator of electro magnetic wave. However this is provided that the frequency of the applied signal corresponds with the wavelength that is twice the length of the slot.
This effect is utilized in the slotted wave guide antenna where a number of vertical slots are cut on one side of the wave-guide itself.
The slots interrupt the pattern of the alternating current flow along the wall of the wave-guide and thus a signal is effectively applied across the centre of each slot.
The slots are cut at equal interval such that the signals all emit out in the same phase. The slotted wave-guide antenna thus constitutes a large number of radiators having a uniform phase distribution across a plane aperture.
This produces a pattern as follows:
Since the wave guide is fed with the alternating signal from one end the horizontal beam width pattern will be rotated by a small amount away from the feed end of the guide, such that the axis of the main lobe will make a horizontal angle of about 3° to 4° with the normal of the slot aperture.
This angle is frequency dependent and is known as the angle of squint.
The slotted wave guide antenna is preferred over other types of antenna because of the ability to produce direct emission and to offer higher aerial gain by reducing the power radiated in the side lobes.