Information
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Patent Grant
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6400311
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Patent Number
6,400,311
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Date Filed
Tuesday, December 19, 200024 years ago
-
Date Issued
Tuesday, June 4, 200222 years ago
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Inventors
-
Original Assignees
-
Examiners
Agents
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CPC
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US Classifications
Field of Search
US
- 342 118
- 342 121
- 342 122
- 342 123
- 342 124
- 342 165
- 342 169
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International Classifications
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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 |