CROSS-REFERENCE TO RELATED APPLICATIONS

Reference is made to a co-pending and commonly assigned patent application entitled A RETROFIT SOLUTION FOR THE INTEGRATION OF GROUND-BASED WEATHER RADAR IMAGES WITH ON-BOARD WEATHER RADAR, Ser. No. 09/645,666, filed Aug. 24, 2000, which is herein incorporated by reference in its entirety.

FIELD OF THE INVENTION

The present invention relates to on-board weather radar for use on aircraft or other vehicles. More particularly, the present invention relates to methods and apparatus for providing ground-based weather radar information to a pilot using on-board weather radar cockpit displays.

BACKGROUND OF THE INVENTION

Weather has been identified as a cause or contributing factor to nearly 25% of aviation accidents and 35% of fatalities. Accidents occur when a chain of events leads to a failure of an aircraft system, a mistake on part of the crew piloting the aircraft, or a combination thereof. Improved levels of weather information and the use of pilot decision aids may be helpful in breaking the chain of events that leads to an accident.

In addition to creating hazardous situations, weather is a common cause of flight delays. For example, in the United States, more than 70% of delays are attributed to weather conditions. While the industry will always have some level of delay caused by extreme weather, there is a growing belief that improved weather information in the cockpit could improve efficiency for the overall system.

On-board weather radar is a tactical navigation aid that shows convective hazards for the next 15 to 30 minutes of flight. The on-board weather radar currently serves as the focus of a pilot's awareness of the weather situation. It provides a graphical depiction of precipitation relative to the aircraft's position. The presence of turbulence can be inferred from these reflections off of precipitation. Through the use of Doppler processing, turbulence can also be detected and displayed directly.

While the on-board weather radar has proven invaluable as a real-time source of tactical weather information, the range is limited. Additionally, the beam width of on-board weather radar increases significantly at longer ranges, making it difficult to perform fine resolution of precipitation patterns.

To enhance safety and efficiency, government and industry are attempting to improve the availability and quality of weather information available to flight crews. It is desirable to provide flight crews with weather information which has been up-linked from a ground-based weather radar system. One such ground-based weather radar system is the Next Generation Weather Radar (NEXRAD) system, the data from which is available via the Internet or other sources. These ground-based weather radar systems offer a strategic view of weather over a larger region than possible with on-board weather radar. The NEXRAD system includes ground-based radar sites distributed across the continental United States. The NEXRAD system is used to create a series of weather products, including base reflectivity, composite reflectivity, hail indices, and storm tracking information, to name a few. Generally, NEXRAD provides an excellent strategic view of the weather situation, but would likely suffer in cockpit applications from latencies due to acquisition, processing and up link.

The pilot community has expressed interest in up-linking ground-based radar images, like those available from NEXRAD, to the cockpit as has been proposed. Several industry-led programs have focused on development of applications for displaying these images in the cockpit of an aircraft. However, as mentioned earlier, these images suffer in cockpit applications from latencies due to acquisition, processing and up-link. On the other hand, the on-board weather radar images do not suffer from latencies but are of limited range. Consequently, a method that utilizes the benefits of both of these two sources would be a significant improvement in the art.

SUMMARY OF THE INVENTION

A radar displaying system and method for use in displaying weather radar information on a cockpit display of an aircraft receiving on-board weather radar information from an on-board weather radar system and ground-based weather radar information up-linked to the aircraft from a ground-based weather radar system. The information from the on-board weather radar system and the information from the ground-based weather radar system are combined to generate composite weather radar information. In response to the composite information, the cockpit display simultaneously displays both on-board weather radar imagery and ground-based weather radar imagery.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1

is a block diagram illustrating a prior art on-board weather radar system.

FIG. 2

is a block diagram illustrating an on-board weather radar system in accordance with the invention which integrates on-board weather radar data with up-linked weather radar data from a ground-based system.

FIG. 3A

is an illustration of prior art on-board weather radar imagery.

FIG. 3B

is an illustration of prior art ground-based weather radar imagery.

FIG. 4A

is an illustration of the display of ground-based weather radar imagery on an on-board weather radar cockpit display in accordance with the present invention.

FIG. 4B

is an illustration of a composite of on-board and ground-based weather radar imagery in accordance with the present invention.

FIGS. 5A-5C

are illustrations of the composite on-board and ground-based weather radar imagery provided by weather radar systems of the present invention.

FIG. 6

is a table illustrating color mapping between ground-based weather radar and on-board weather radar in accordance with some embodiments of the invention.

DETAILED DESCRIPTION OF AN ILLUSTRATIVE EMBODIMENT

FIG. 1

is a block diagram illustrating a prior art weather radar system

100

. System

100

includes radome

110

, antenna (shown with mount)

115

, receiver/transmitter

120

, controller

130

and cockpit display

140

. Under the control of controller

130

, receiver/transmitter

120

transmits a radar pulse through antenna

115

and radome

110

in one particular direction at a time. The radar pulse travels outward from the aircraft in the particular direction and reflects off of precipitation or other weather phenomena. As reflections come back and are received by antenna

115

and receiver/transmitter

120

, an indication of the weather at different distances (out to a range) along a straight line in the particular direction can be ascertained. The data that is received by receiver/transmitter

120

is put into a data stream and provided to cockpit display

140

for displaying weather radar information to the pilot. As antenna

115

sweeps back and forth, data for hundreds of these “radials” are obtained every sweep, thus providing a complete picture of the weather in front of the aircraft. A radial can be defined as weather radar information along a line, out to a range, for a given tilt angle and scan angle from the aircraft as is known in the art.

In conventional on-board weather radar systems, the data that is received is frequently put into an ARINC

453

weather radar data structure, for example ARINC CHARACTERISTIC

708

A. Each word of this data structure includes data representing the intensity of the weather at a multiplicity of points along the straight line of a radial out to a range, which is typically no greater than about 100 miles. The intensity data for each of the points represented in the ARINC

453

word is stored in range bins of the word. The ARINC

453

word also includes header information indicative of the range and direction for the radial.

FIG. 3A

is a representation of an on-board weather radar image

300

of the type which is typically displayed by cockpit display

140

of system

100

shown in FIG.

1

. Based upon the color of different pixels or areas shown in image

300

, the pilot of the aircraft (aircraft represented graphically at

305

) can determine the intensity and direction of weather conditions or phenomena ahead of the aircraft. As shown in

FIG. 3A

, on-board weather radar typically provides an accurate indication of weather conditions to a range of approximately 100 miles from the aircraft. Given the high travel speeds which are typical of many aircraft, this can represent as little as ten or fifteen minutes of travel.

FIG. 3B

illustrates ground-based weather radar image

320

which is available from a weather information service provider. Image

320

represents a prior art NEXRAD bit map or graphical representation of weather.

FIG. 2

is a block diagram illustrating weather radar system

200

adapted for use on an aircraft in accordance with the present invention. Weather radar system

200

combines on-board weather radar information with up-linked, ground-based weather radar information, displaying them simultaneously on the same display. This provides pilots with both real-time tactical information and longer-range strategic views. As will be discussed below in greater detail, the concept is applicable to dedicated weather radar indicators, to existing Electronic Flight Instrument PATENT System (EFIS) based weather radar displays, and to yet to be developed display hardware. Further, in some embodiments, weather radar system

200

is adapted to provide ground-based weather radar images (for example see FIG.

4

A), without being integrated on-board weather radar images, on these existing indicators or displays.

Referring back to embodiments in which on-board weather radar information is displayed simultaneously with ground-based weather radar information on the same indicator, the co-display of the two radar images utilizes the strengths of the two sources of information. The on-board radar provides a real-time view of the weather within close range to the aircraft—where the pilot needs real-time information. The NEXRAD (or other ground-based radar) data, on the other hand, cannot be considered real-time for this aviation application. There are delays due to the time required in processing, distributing and transmitting the data. However, NEXRAD data can be displayed for the longer ranges, providing information beyond the range of the on-board radar. At these ranges, the age of the data is not as critical.

System

200

includes radome

110

, antenna

115

, receiver/transmitter

220

, controller

230

, cockpit display

240

, pilot input device

242

, data link or communication system

250

, and weather radar data integration circuitry

260

. System

200

also utilizes position/heading information provided from a position/heading determining system

270

, which can be for example a Global Positioning System (GPS) receiver.

Controller

230

, receiver/transmitter

220

and antenna

115

function substantially or identically to the manner in which the similar components in system

100

function. Thus, under the control of controller

230

, receiver/transmitter

220

sequentially transmits pulses through antenna

115

in each of a large number of directions to obtain information

222

for multiple radials required to produce an on-board weather radar image such as image

300

shown in FIG.

3

A. This information

222

is provided to weather radar data integration circuitry

260

, which can be a suitably programmed processor or other circuitry. As will be discussed below in greater detail, integration circuitry

260

can be existing circuitry, in retrofit radar systems, adapted or programmed to implement the functions of the present invention.

Data link

250

is a communication system which is adapted to receive up-linked weather radar data

252

from a ground-based weather radar system and to provide this ground-based weather radar data to weather radar data integration circuitry

260

. For example, the up-linked ground-based weather radar data can be received from a ground-based transmitter which obtains the weather radar data from the internet or from other sources. In exemplary embodiments, the ground-based weather radar information

252

includes data representative of a NEXRAD image in a format such as the bit map (BMP) or Graphic Interchange Format (GIF) formats.

FIG. 3B

illustrates an image

320

of this type.

Using position and heading information

272

provided by position/heading determining system

270

, weather radar data integration circuitry

260

determines the relevant portion of the up-linked ground-based weather radar data

252

for the current position and heading of the aircraft. In other words, based on the position and heading of aircraft

305

, data integration circuitry

260

can extract from the total up-linked ground-based weather radar data

252

the portions corresponding to the radials obtained by the on-board radar (see FIG.

3

A). However, these portions will typically extend to a range beyond the range obtained by the on-board radar system, and only data corresponding to selected ranges need be identified.

Data integration circuitry

260

combines the on-board weather radar data

222

with the ground-based weather radar data

252

and produces composite weather radar data

262

which is provided to cockpit display

240

. Using composite weather radar data

262

, cockpit display

240

provides display images such as image

400

shown in FIG.

4

B. As can be seen in

FIG. 4B

, using data

262

, cockpit display

240

displays composite radar image

400

with both on-board weather radar imagery

402

and ground-based weather radar imagery

404

shown together relative to a position of the aircraft represented at

305

. The on-board weather radar imagery

402

illustrates weather information for positions which are closer to the aircraft, while ground-based weather radar imagery

404

illustrates weather information at positions further from the position of the aircraft.

Pilot input device

242

is used by the pilot to control cockpit display

240

. For example, using input device

242

, the pilot can change the range of displayed information. Simultaneously providing on-board weather radar imagery for the near ranges and ground-based weather radar imagery for the outer ranges, on a single weather radar cockpit display, is a highly beneficial tool for the pilot of the aircraft. In some embodiments, input device

242

can be used to control cockpit display

240

such that only ground-based weather radar imagery is shown.

FIG. 4A

is an illustration of the display on cockpit display

240

of only ground-based weather radar imagery

350

in accordance with the these embodiments of the present invention. If the on-board radar system is adapted to utilize a pre-existing data structure, such as the ARINC

453

data structure, ground-based weather radar imagery

350

can be provided by encoding ground-based weather radar data

252

onto a ARINC

453

data bus. It must be noted that the present invention is not limited to ARINC

453

data bus embodiments.

The images shown in

FIGS. 3A and 4A

represent the same weather pattern, with image

300

(

FIG. 3A

) showing the weather pattern as determined from on-board radar and image

350

(

FIG. 4A

) representing the weather pattern as determined from ground-based radar. As can be seen, the ground-based radar provides greater weather detail at certain ranges. In this example, the aircraft was flying at 22,000 feet. By comparing

FIGS. 3A and 4A

, it can be seen that the NEXRAD image

350

includes precipitation which is underneath the view of the on-board radar. Also, notice that as the range increases outward, the on-board radar detects more of the precipitation shown in the NEXRAD image. This is due to the increasing beam width of the on-board radar as a function of distance from the aircraft. Since the NEXRAD image

350

provides weather information which is not available in the on-board radar image

300

, it is desirable to provide this information to the pilot of the aircraft. However, as discussed previously, limited panel real estate in the cockpit of most aircraft renders it difficult to install new displays which support bitmap type images such as are typically used to display NEXRAD images in non-aviation environments. Therefore, the methods of the present invention which allow ground-based weather radar information and on-board weather radar information to be displayed using the same cockpit displays are highly desirable.

Referring back to

FIG. 4B

, also illustrated in greater detail is portion

410

of image

400

. As can be seen more clearly in portion

410

which is enlarged for ease of illustration, image

400

includes delineating symbology or graphical separator

420

positioned between on-board weather radar imagery

402

and ground-based weather radar imagery

404

. Separator

420

provides an indication, which is quickly discernable by the pilot of the aircraft, of which portions of display image

400

correspond to on-board weather radar imagery

402

and which portions correspond to ground-based weather radar imagery

404

.

FIGS. 5-A

,

5

-B and

5

-C provide additional illustrations of composite radar images which can be displayed on cockpit display

240

in accordance with the present invention. In

FIG. 5A

, composite image

500

is shown, with on-board weather radar imagery

502

shown in the lower central regions of the image, and with the ground-based radar imagery

504

shown in the upper and outer portions of the image. In this embodiment, delineating symbology

520

, which separates imagery

502

from imagery

504

, is a solid line instead of a dashed line. Also, as shown in

FIG. 5A

, symbology

520

can include data

522

indicating the age of the ground-based weather radar data. Data

522

can be positioned on or in close proximity to symbology

520

as illustrated, or can be positioned elsewhere on image

500

.

FIGS. 5B and 5C

illustrate image

550

showing composite weather radar information at two separate ranges relative to a position of the aircraft (reference at

555

). In

FIG. 5B

, on-board weather radar imagery

552

is shown relative to ground-based weather radar imagery

554

, with the total range of composite weather radar information extending to approximately 400 miles. As can be seen by the position of delineating symbology

570

, the range of the on-board weather radar information is approximately 100 miles out of the 400 mile total range. This view provides the pilot of the aircraft with greater long-range strategic weather information.

In contrast, in

FIG. 5C

, the same image

550

is shown, but with the range limited to approximately 160 miles. Thus, in the view shown in

FIG. 5C

, the portion of screen of cockpit display

240

used to show on-board weather radar imagery

552

increase, while the portion of the cockpit display screen used to illustrate ground-based weather radar imagery

554

decreases. Thus, this view provides the pilot with more detailed short-range tactical weather radar information. Generally, the pilot of the aircraft would control the total composite range, and thereby control the short-range and long-range weather radar data detail, using a pilot input device

242

(shown in FIG.

2

). Further, in some embodiments of the present invention, the pilot uses input device

242

to control not only the total range of the composite radar image, but also the total range of the on-board radar portion of the image. At one extreme, the pilot can reduce the range of displayed on-board radar data to zero such that the cockpit display displays only ground-based radar data, for example as shown in FIG.

4

A.

An important issue which must be addressed in the combining of ground-based weather radar data with on-board weather radar data relates to color mapping. Ground-based weather products often use a different color standard than that used in airborne radar. However, many experts suggest that the colors (for example black, green, yellow and red) of the radar image should represent the same thing for the pilot, regardless of the source. In one embodiment of the present invention, the sixteen NEXRAD intensity (color) levels are mapped to the four colors (black, green, yellow and red) of an exemplary conventional on-board weather radar system. The mapping in this embodiment can be accomplished using the relationships illustrated in Table 1 shown in FIG.

6

.

The mapping specified in Table 1 causes loss of some of the information originally contained in the NEXRAD (or other ground-based weather radar) image. However, by making this conversion on the ground, prior to transmission to the aircraft, the bandwidth requirements for the up-linked images can be halved. Thus, by converting prior to transmission, each pixel will require two bits of data, rather than four bits. By using a compression method, like run-length encoding, the bandwidth requirements can be reduced even further.

Although the present invention has been described with reference to illustrative embodiments, workers skilled in the art will recognize that changes may be made in form and detail without departing from the spirit and scope of the invention.