Radar rangefinder

Information

  • Patent Grant
  • 6400311
  • Patent Number
    6,400,311
  • Date Filed
    Tuesday, December 19, 2000
    23 years ago
  • Date Issued
    Tuesday, June 4, 2002
    22 years ago
Abstract
The inventive radar rangefinder has a transmitting/receiving antenna (22) for surveying a danger area. Said antenna is located in a radome housing (12), on a rotatable platform (18). A reflector is placed at a known distance in order to calibrate the device. This reflector is formed by an auxiliary antenna (24) with a connected delay line (26) inside the randome housing (12). The length of the virtual distance of the reflector produced then corresponds to the velocity factor of the delay line used.
Description




The present invention relates to a radar rangefinder as claimed in the descriptive part of patent claim 1.




Such a radar rangefinder is used, for example, in an arrangement for monitoring a danger area, as is illustrated and described in DE 196 12 579 A1 from the same applicant.




In the FMCW radar (frequency-modulated continuous-wave radar) used there, temperature-dependent and age-dependent changes normally prevent a desired strictly linear frequency/time function. The voltage-controlled oscillators in the available transmitters have non-linear drive characteristics which are highly dependent on temperature, load and the operating voltage.




In this context, it is known for calibration methods to be used, which use a target which produces an echo at a known distance. This allows self-calibration to be carried out, using the Hilbert transformation. However, the arrangement of a target which produces an echo at a known distance has various disadvantages. Firstly, this target can be concealed by people or objects moving in the area. Secondly, raindrops, snow or ice in the measurement path or on the radome housing in which the radar rangefinder is arranged can adversely affect the calibration. On the other hand, it is desirable for the calibration distance to be as great as possible in order to keep the calibration measurement error as small as possible.




Against this background, the object of the present invention is to specify a radar rangefinder having a reflector for calibration, in which the disturbance influences mentioned above are all precluded.




This object is achieved according to the distinguishing features of patent claim 1. Further advantageous refinements of the radar rangefinder according to the invention can be found in the dependent claims.




The invention will be described in more detail in the following text with reference to an exemplary embodiment which is illustrated in the figures of the attached drawing, in which:











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

shows the principle of the design of the radar rangefinder according to the present invention; and





FIGS. 2 and 3

show a block diagram of the components used in the radar rangefinder shown in FIG.


1


.











DETAILED DESCRIPTION OF THE INVENTION




According to

FIG. 1

, a fixed-position basic unit


14


with associated electronics


16


and a rotating platform


18


is arranged in a protective cover


12


, which is arranged on a base


10


and is referred to in the following text as a radome housing, and the rotating platform


18


is fitted with a radar transmitting/receiving antenna


22


with associated electronics


20


. A horn antenna


24


is arranged inside the radome housing


12


such that, when the transmitting/receiving antenna


22


rotates through 360°, the horn antenna


24


is painted in an angle region which is located outside the danger area monitored by the transmitting/receiving antenna


22


. A patch antenna could also be used instead of a horn antenna. The transmitting/receiving antenna


22


may also be rotated to a position where it faces the horn antenna


24


, for calibration. A delay line


26


is connected to the horn antenna


24


and is short-circuited at its end, dictating a specific shortening factor. Thus, for example, a delay line


26


with a length of about 8 m corresponds to an electrical length of 20 m, so that this results in conditions as if the target which produces the echo were arranged at a distance of 20 m. The delay line


26


is routed upward into the dome


28


of the radome housing


12


, where it is wound up in turns. The delay line


26


may be formed by a round waveguide or a rectangular waveguide.





FIGS. 2 and 3

show those components which are located inside the radome housing


12


on the stationary base unit


14


and the rotating platform


18


.

FIG. 2

shows the end of the delay line


26


short circuited while

FIG. 3

shows the end of the delay line


26


open-circuited.




The rotating platform


18


is driven by a motor


30


, which is driven by a control module


32


via a position regulator


34


and a power output stage


36


. A resolver


38


forms an actual value signal for the position regulator


34


. A power supply unit


40


, which is connected to the power supply via an EMC filter


42


, supplies the required regulated DC voltage. The voltage supply for the rotating platform


18


as well as a communications interface for incoming and outgoing data are provided via a slipring arrangement


44


.




The rotating platform


18


is fitted with the transmitting/receiving antenna


22


, an RF transmitting/receiving module


46


, which has a preamplifier


48


and a voltage-controlled transceiver


50


, as well as a digital signal processor module


52


, which comprises an A/D and D/A converter


54


and the actual signal processor


56


.




The danger area to be monitored is bounded by three triple mirrors


58


,


58


′,


58


″, and a target object


60


is to be detected in this area. The horn antenna


24


and the delay line


26


are arranged on the inner wall inside the radome housing


12


.



Claims
  • 1. A radar rangefinder comprising: a transmitting/receiving antenna arranged on a rotating platform for monitoring a danger area, a radome housing for accommodating the transmitting/receiving antenna, and a reflector arranged at a known distance in order to preset a calibration for the rangefinder, wherein:a) the reflector is provided by an auxiliary antenna, which is likewise arranged in the radome housing; b) the auxiliary antenna is coupled to a delay line, the delay line having a shortening factor, an actual length, a virtual length, and an end, the end of the delay line being coupled to the housing; c) the delay line is arranged together with the auxiliary antenna on an inner wall of the radome housing; and d) the virtual length of the delay line is greater than the actual length of the delay line.
  • 2. The radar rangefinder as claimed in claim 1, wherein the auxiliary antenna is arranged in an angle region outside the measurement range.
  • 3. The radar rangefinder as claimed in claim 2, wherein the auxiliary antenna is a horn antenna.
  • 4. The radar rangefinder as claimed in claim 2, wherein the auxiliary antenna is a patch antenna.
  • 5. The radar rangefinder of claim 1, wherein the transmitting/receiving antenna is moved to a position where is faces the auxiliary antenna for calibration.
  • 6. The radar rangefinder as claimed in claim 1, wherein the calibration is carried out during rotation of the transmitting/receiving antenna.
  • 7. The radar rangefinder as claimed in claim 1, wherein the delay line is arranged in a winding in a dome of the radome housing.
  • 8. The radar rangefinder as claimed in claim 7, wherein the delay line is provided by means of a round waveguide with a short circuit.
  • 9. The radar rangefinder as claimed in claim 7, wherein the delay line is provided by a rectangular waveguide with a short circuit at the end.
  • 10. The radar rangefinder as claimed in claim 7, wherein the delay line is provided by means of a round waveguide with a open circuit.
  • 11. The radar rangefinder as claimed in claim 7, wherein the delay line is provided by a rectangular waveguide with a open circuit at the end.
Priority Claims (1)
Number Date Country Kind
198 13 631 Mar 1998 DE
PCT Information
Filing Document Filing Date Country Kind
PCT/EP99/01979 WO 00
Publishing Document Publishing Date Country Kind
WO99/50686 10/7/1999 WO A
US Referenced Citations (1)
Number Name Date Kind
4245221 Kipp et al. Jan 1981 A
Foreign Referenced Citations (1)
Number Date Country
2105942 Mar 1983 GB