This application claims priority from U.K. Patent Application No. 1605439.7, filed Mar. 31, 2016 and European Patent Application No. 16290039.3, filed Feb. 18, 2016. The disclosures of both applications are incorporated herein by reference.
This invention relates to a radar apparatus, and to a method of operating such apparatus.
Radar apparatus, especially for automotive applications such as automatic cruise control or automatic emergency braking, are well known. Generally, they comprise a source of radar signals, a transmitter for the radar signals, and reception and processing apparatus. Such a system is known from, for example, the PCT patent application published as WO2004/053521.
However, particularly where such radar apparatus are deployed in such harsh environments as the engine compartment of an automobile, they necessarily only have a finite temperature range in which they will operate. Typically, above a limit, say 85 degrees centigrade, it is necessary to cease operation of the circuit, as it will either not function correctly, or may even become damaged so that it is not operational when the temperature returns to within its normal operating range. Furthermore, continued operation can itself make the temperature problem worse, as such radar apparatus generate heat during operation; if operated at a temperature above the normal operating range, the heat produced may further increase the temperature thus reinforcing the deleterious effects of the high temperatures.
According to a first aspect of the invention, there is provided a radar apparatus, comprising:
As such, we have appreciated that a functional radar apparatus can still be achieved that can function at higher temperatures than otherwise would be the case by reducing the power transmitted at higher temperatures, potentially avoiding or at least partially ameliorating at least some of the deleterious effects described above. The inventors have appreciated that a radar apparatus will still function sufficiently well at low power to be useful.
In one embodiment, the first and second temperature ranges may be adjacent (in that the highest temperature of the first temperature range may be the same as the lowest temperature of the second temperature range). Alternatively, there may be a third temperature range between the first and second temperature ranges. The signal generation unit may be arranged so as to decrease the output power as the output signal indicates a temperature increasing through the third range, typically from the first power to the second power, and typically linearly.
The second power may be 3 decibels less than the first power, to within 0.5, 0.25 or 0.1 decibels. Typically, the highest temperature in the first range may be between 80 and 90 degrees Celsius, typically around 85 degrees Celsius (±1 degree).
Additionally, the signal generation unit may be arranged so as to cease generating radar signals should the output signal indicate a temperature above a threshold, the threshold typically being higher than the second range.
The radar apparatus may comprise a transmitter for the radar signals, coupled to the output of the signal generation unit. Typically, the transmitter will comprise at least one antenna. Each antenna may be a planar patch antenna. The transmitter may have a transmission pattern such that, at a given field strength, the radar signals are transmitted less far but over a wider angular field at the second power than at the first power.
The radar apparatus may also comprise a receiver for receiving radar signals (received radar signals), which may comprise at least one receiving antenna. Typically, the radar apparatus may comprise a reception unit which is arranged to detect and process the received radar signals.
According to a second aspect of the invention, there is provided a method of operating a radar apparatus, comprising:
As such, we have appreciated that a functional radar apparatus can still be achieved that can function at higher temperatures than otherwise would be the case by reducing the power transmitted at higher temperatures. The inventors have appreciated that a radar apparatus will still function sufficiently well at low power to be useful.
In one embodiment, the first and second temperature ranges may be adjacent (in that the highest temperature of the first temperature range may be the same as the lowest temperature of the second temperature range). Alternatively, there may be a third temperature range between the first and second temperature ranges. The method may comprise decreasing the output power as the temperature increases through the third range, typically from the first power to the second power.
The second power may be 3 decibels less than the first power, to within 0.5, 0.25 or 0.1 decibels. Typically, the highest temperature in the first range may be between 80 and 90 degrees Celsius, typically around 85 degrees Celsius (±1 degree).
Additionally, method may comprise ceasing to generate radar signals should the output signal indicate a temperature above a threshold, the threshold typically being higher than the second range.
The method may comprise transmitting the radar signals, typically using at least one antenna. Each antenna may be planar patch antenna. The antenna(s) may have a transmission pattern such that, at a given field strength, the radar signals are transmitted less far but over a wider angular field at the second power than at the first power.
The method may also comprise receiving received radar signals, typically using at least one receiving antenna. Typically, the method may comprise detecting and processing the received radar signals.
The method may comprise the use of the radar apparatus of the first aspect of the invention.
Various aspects of this invention will become apparent to those skilled in the art from the following detailed description of the preferred embodiment, when read in light of the accompanying drawings.
A radar apparatus in accordance with a first embodiment of the invention is shown in
The transmission antenna 3 is arranged to transmit the radar signals to an area where there may be targets 4. Radar signals reflected off the targets 4 are received by a reception antenna 5 and processed by a reception circuit 6 and passed to a mixer 7, which downmixes the received radar signals with a portion of the generated radar signal for processing by a processor 8.
A control unit 9 such as a microprocessor controls the operation of the radar apparatus. The radar apparatus is housed within a housing 11. The radar apparatus is also provided with a temperature sensor 10, such as a thermocouple. This is used to determine the temperature of part of the radar apparatus, for example the housing 11 or alternatively the signal generation unit 1. In order to still allow the radar apparatus to function at all above its otherwise usual high temperature limit, the control unit 9 controls the signal generation unit 1 to reduce the power of the signals generated by the signal generation unit 1 at high temperatures, as shown in
Above the second range—so above 105° C., the signal generation unit 1 ceases operating. This value of 105° C. is higher than would have previously been achieved with the same circuit operating at full power.
The inventors have appreciated that even at reduced transmission power, useful results can be had from the radar apparatus. This can be seen in
In
The following table shows the maximum ranges for the different detected elements at full and low power:
This still gives useable results, even when reducing the power to avoid the effects of overheating.
The principle and mode of operation of this invention have been explained and illustrated in its preferred embodiment. However, it must be understood that this invention may be practiced otherwise than as specifically explained and illustrated without departing from its spirit or scope.
Number | Date | Country | Kind |
---|---|---|---|
16290039.3 | Feb 2016 | EP | regional |
1605439.7 | Mar 2016 | GB | national |