Technical background When positioning a land-based radar which purpose is to scan the horizon around a geographical site, it is often practical to know at which elevation to start scanning.

This way one can avoid spending time scanning directly into e. g. mountains.

One possible solution is for the radar to initiate a search in elevation (e. g. from the highest allowed elevation and down) for the horizon, typically on a sector-by-sector basis, and detect where the ground clutter level starts to be significant.

A radar can get a certain amount of false echo above the horizon (e. g. birds, second-time-around echo from distant planes, etc) which may set the horizon higher than necessary. Sometimes radar echo are also sufficiently absorbed by surrounding terrain so that the horizon may be set lower than required.

Rain, snow and fog can also affect such a measurement.

In addition a radar often has a minimum range of detection.

This result in objects which constitute part of the horizon and being"too close"blocks the view without the radar detecting this.

Another important issue in military applications is Electronic Warfare where radar silence is an important counter measure. This means that search elevation have to be found without using the radar actively.

Brief summary of the invention Thus, it is an object of the present invention to provide a method for evaluating the terrain around a radar site that is quickly performed without relying on the radio properties of the radar installation.

Another object is to provide a method that can be performed without betraying the presence of the radar.

These objects are met by a method as defined in the appended patent claims. In essence, the method comprises to calculate the radar horizon around a radar site from stored terrain elevation information.

Brief description of the drawings The invention will now be described in detail in reference to the appended drawings, in which Fig. 1 is a diagram showing a sector of the terrain around a radar site and the positions of the points in which the elevation of the terrain is calculated.

Fig. 2 is a schematic view of a radar installation with the necessary equipment for performing the inventive method.

Fig. 3 is a flow diagram showing the individual steps performed in the inventive method.

Fig. 4 is the resultant radar horizon in front views.

Fig. 5 is a section along one of the sectors in Fig. 4, illustrating how the resultant profile is obtained.

Detailed description of the invention.

The invention consists of a method for evaluating a radar horizon around a radar site. The radar can then import this information and use it for setting up a scanning pattern that avoids the transmission of energy into the surrounding terrain.

The method is performed on a computer that, from a given position, divides the surrounding terrain into sectors. In each sector a number of calculation points are chosen, based on simple geometrical considerations.

In each calculation point the radar search elevation angle is calculated from terrain altitude information stored in a database. Fig. 2 shows the process. The computer consults the database for each calculation point. If the angle is greater than the previous angle in the current sector, then this angle is stored as the greatest angle. The reason for this is that a nearby object, e. g. the small hill, might "shadow"a larger object farther away, e. g. a mountain in the distance. The stored angle is lowest angle the sweeping ray may use in order to clear the terrain in this sector.

The suite of stored angles for all sectors considered constitutes a"radar horizon"for this particular site. The calculated horizon can then be presented for the radar operator and the radar scanning pattern can be adjusted accordingly, either automatically (i. e. directly), manually (i. e. operator confirmed) or semi-automatically (i. e. directly but where the operator can adjust manually at a later time).

The calculation is performed either as a separate program or as part of an already existing program on the computer where access to a suitable set of terrain altitude data on a digital format is required. This terrain data, e. g. DTED, can be stored in a conventional or proprietary database, preprosessed or otherwise, or in raw DTED format outside of, but connected to, the invention (DTED: Digital Terrain Elevation Data, METRIC MIL-PRF-89020A).

The latter is particularly ideal as it provides for the user of the invention to add further terrain data with the detailing level for the area of interest without requiring a separate tool.

Figure 1 shows how the calculation points are chosen within a sector. Near to the radar site, the altitude is fetched from the database in points along a line going outward from the site. Whenever the distance between an edge of the sector and the nearest point grows too great the number of calculation branches is increased by one. When branching occurs, the calculated values in parallel points (i. e. in points at the same range in parallel branches) are compared, and the highest value chosen as the value representing this particular range.

In particular the following parameters are considered: Absolute geographical position of origo Sector width Number of sectors (ie. the total view) Azimuth offset Max sector range; the length of each sector from the observation point Stepsize ; the distance between each sampled point from the altitude database (LSB in Fig. 1). The stepsize is chosen dependent on the resolution in the altitude database and the general calculation performance desired.

From these initial parameters the following is calculated: Number of calculations (steps) in one path ; this value is calculated from the stepsize and sector width parameters in the input data. Each look up in the altitude database is done for every step length along a path (or a line) inside the sector until the stepsize limit is reached. The stepsize limit is reached when the width of the sector is greater than the horizontal cell size in the altitude database.

Number of branches ; this value is calculated from the stepsize, max sector range and stepsize parameters in the input data. When the stepsize limit is reached for all existing parallel paths (if any) then the algorithm performs a branch which means that the number of parallels is increased by one.

Number of parallel calculation paths ; this value is calculated from the stepsize parameter in the input data. When the look-ups in the altitude database for the parallel paths do not cover the width of the subsector, it is increased by one. The parallel paths have the same azimuth and number of calculations on the path, but displacement sideways is different.

'Displacement ; a function of the previous parameter.

Fig. 3 shows visualizes the individual steps performed in the procedure for evaluating a site.

A geographical point is calculated by looping through, in nested order, the number of branches, number of paralells and number of steps. For each point the following procedure is performed: Based on the azimut, the range and the displacement a transformation from polar to Cartesian coordinates is performed. This gives a geographical coordinate relative to origo. For this point the terrain altitude is retrieved from the height database (see fig. 2). This altitude is stored in the side-view terrain profile, if it is the highest altitude for this range. The elevation is then calculated as: arctan (altitude/range) and is then compared to the previous highest elevation for the sector. If it is the highest it is stored in a front- view terrain profile, Fig. 4.

This procedure is the repeated for all points and for all branches for the specified sector. The end result can visually be presented like in Fig. 5.

The view in fig. 5 is of the left-most sector in fig. 4.

The visibility here is limited by a nearby obstruction.

The invention can be used for evaluating possible radar sites, e. g. when placing a radar installation for an airport. It allows for off-site evaluation of the terrain.

Thereby multiple sites can be evaluated and the best located.

The method can also be performed"on the fly"when relocating a mobile radar. In this application the vertical profile shown in Fig. 4 is of particular usefulness, as it can indicate for the operator that a better place can be found in the immediate neighborhood.

Another possible application is to use the method for automatically guiding a mobile unit, e. g. a vessel, car or airplane, to the"best"sites along its course.

However, the main application will be in establishing a scanning horizon for a radar when it has been installed at its site. In this respect one obtains the advantage of eliminating the problems of determining why an echo has not returned and whether it has returned for the"wrong" reasons.