Aircraft groundspeed measurement system and technique

Claim 2

An aircraft groundspeed measurement system comprising: means for transmitting a radar signal from an aircraft towards a target area; first means for receiving reflected radar return signals from a target area vertically beneath an aircraft and providing an output representing aircraft altitude; second means for receiving reflected radar return signals from a target area at a slant angle forward of the aircraft and providing an output representing aircraft slant velocity along said slant angle and aircraft slant range to said target area along said slant angle; and means responsive to said output representing altitude, slant range, and slant velocity, for calculating and providing an output signal representing aircraft groundspeed for a mathematical relationship correlating said altitude, slant range and slant velocity.

Claim 3

An aircraft groundspeed measurement system comprising: means for providing a modulating signal; means responisve to said modulating signal for generating a variable frequency signal; means for transmitting said variable frequency signal from an aircraft to a target area beneath the aircraft; first means for receiving reflected returns of said variable frequency signal from a first target area vertically beneath an aircraft; second means for receiving reflected returns of said variable frequency signal from a second target area at a slant angle forward of an aircraft; third means coupled to said first means for mixing a portion of said variable frequency signal with said received reflected returns from said first target area to produce a beat frequency and providing an output representing aircraft altitude; fourth means coupled to said second means for mixing a portion of said variable frequency signal with said received reflected returns from said second target area to produce a beat frequency and providing outputs representing aircraft slant range to the target area forward of said aircraft along the slant angle and aircraft slant velocity along the same slant angle; and

Claim 4

An aircraft groundspeed measurement system comprising: means for providing a modulating signal; means responisve to said modulating signal for generating a variable frequency signal; means for transmitting said variable frequency signal from an aircraft to a target area beneath the aircraft; first means for receiving reflected returns of said variable frequency signal from a first target area vertically beneath an aircraft; second means for receiving reflected returns of said variable frequency signal from a second target area at a slant angle forward of an aircraft; third means coupled to said first means for mixing a portion of said variable frequency signal with said received reflected returns from said first target area to produce a beat frequency and providing an output representing aircraft altitude; fourth means coupled to said second means for mixing a portion of said variable frequency signal with said received reflected returns from said second target area to produce a beat frequency and providing outputs representing aircraft slant range to the target area forward of said aircraft along the slant angle and aircraft slant velocity along the same slant angle; and

Claim 5

An aircraft groundspeed measurement system comprising: means for transmitted a radar signal from an aircraft towards a target area wherein said means for transmitting includes a transmitting antenna having a first predetermined beamwidth; first means for receiving reflected radar return signals from a target area vertically beneath an aircraft and providing an output representing aircraft altitude wherein said first means includes an antenna having a beamwidth equal to said first predetermined beamwidth; second means for receiving reflected radar return signal from a target area at a slant angle forward of the aircraft and providing an output representing aircraft slant velocity along said slant angle and aircraft slant range to said target area along said slant angle wherein said second means includes an antenna having a beamwidth substantially less than said first predeterimed beamwidth; and means responisve to said output representing altitude, slant range, and slant velocity, for calculating and providing an output signal representing aircraft groundspeed.

Claim 6

An aircraft groundspeed measurement system comprising: means for transmitted a radar signal from an aircraft towards a target area wherein said means for transmitting includes a transmitting antenna having a first predetermined beamwidth; first means for receiving reflected radar return signals from a target area vertically beneath an aircraft and providing an output representing aircraft altitude wherein said first means includes an antenna having a beamwidth equal to said first predetermined beamwidth; second means for receiving reflected radar return signal from a target area at a slant angle forward of the aircraft and providing an output representing aircraft slant velocity along said slant angle and aircraft slant range to said target area along said slant angle wherein said second means includes an antenna having a beamwidth substantially less than said first predeterimed beamwidth; and means responisve to said output representing altitude, slant range, and slant velocity, for calculating and providing an output signal representing aircraft groundspeed.

Claim 7

The system of claim 3 wherein said means for transmitting a radar signal comprises: means for providing a triangular modulating signal having an upsweep and a downsweep; means responsive to said triangular modulating signal for generating a variable frequency output signal; and means for transmitting said variable frequency output signal to said target area.

Claim 8

The system of claim 4 wherein said second means for receiving reflected return signals comprises means for detecting reflected return signals on the downsweep of said triangular modulating signal, and means for detecting reflected return signals on the upsweep of said triangular modulating signal.

Claim 9

The system of claim 4 wherein said second means for receiving the reflected return signals comprises: an antenna for receiving return signals reflected from said target area forward of an aircraft; means coupled to said antenna for mixing a portion of said received reflected return signals with said transmitted variable frequency output signal to produce a beat frequency; means for detecting the beat frequency produced during the downsweep of said triangular modulating signal; and means for detecting the beat frequency produced during the upsweep of said triangular modulating signal.

Claim 10

The system of claim 6 wherein said means for calculating includes means for subtracting the beat frequency produced on the upsweep of the triangular modulating signal from the beat frequency produced on the downsweep of the triangular modulating signal, and means for summing the beat frequency produced on the downsweep of the triangular modulating signal with the beat frequency produced on the upsweep of the triangular modulating signal.

Claim 11

The apparatus of claim 3 wherein said means for calculating further comprises means for correcting said groundspeed output signal to compensate for variations caused by changes in the vertical velocity of an aircraft and the slant angle of reflected returns received from said target area forward of an aircraft.

Claim 12

The system of claim 3 further including means responsive to said output signal representing groundspeed for displaying a visual indication of groundspeed.

Claim 13

The system of claim 3 wherein said means for transmitting a radar signal comprises means for generating a variable frequency signal and means for transmitting said varaible frequency signal to said target area.

Claim 14

The system of claim 3 wherein siad means for transmitting a radar signal and said first means for receiving a reflected radar return signal comprises an FMCW radar altimeter.

Claim 15

An aircraft groundspeed measurement system comprising: means for providing a modulating signal; means responsive to said modulating signal for generating a variable frequency signal; means for transmitting said variable frequency signal from an aircraft to a target area beneath the aircraft wherein said means for transmitting includes an antenna having a first predetermined beamwidth; first means for receiving reflected returns of said variable frequency signal from a first target area vertically beneath an aircraft wherein said first means includes an antenna having a beamwidth equal to said first predetermined beamwidth; second means for receiving reflected returns of said variable frequency signal from a second target area at a slant angle forward of an aircraft wherein said second means inlcudes an antenna having a beamwidth substantially less than said first predetermined beamwidth; third means coupled to said first means for mixing a portion of said variable frequency signal with said received reflected returns from said first target area to produce a beat frequency and providing an output representing aircraft altitude; fourth means coupled to said second means for mixing a portion of said variable frequency signal with said received reflected returns from said second target area to produce a beat frequency and providing outputs representing aircraft slant range to the target area forward of said aircraft along the slant angle and aircraft slant velocity along the same slant angle; and means responsive to said outputs representing aircraft altitude, aircraft slant velocity, and aircraft slant range for calculating and providing an output signal representing aircraft groundspeed.

Claim 16

An aircraft groundspeed measurement system comprising: means for providing a modulating signal; means responsive to said modulating signal for generating a variable frequency signal; means for transmitting said variable frequency signal from an aircraft to a target area beneath the aircraft wherein said means for transmitting includes an antenna having a first predetermined beamwidth; first means for receiving reflected returns of said variable frequency signal from a first target area vertically beneath an aircraft wherein said first means includes an antenna having a beamwidth equal to said first predetermined beamwidth; second means for receiving reflected returns of said variable frequency signal from a second target area at a slant angle forward of an aircraft wherein said second means inlcudes an antenna having a beamwidth substantially less than said first predetermined beamwidth; third means coupled to said first means for mixing a portion of said variable frequency signal with said received reflected returns from said first target area to produce a beat frequency and providing an output representing aircraft altitude; fourth means coupled to said second means for mixing a portion of said variable frequency signal with said received reflected returns from said second target area to produce a beat frequency and providing outputs representing aircraft slant range to the target area forward of said aircraft along the slant angle and aircraft slant velocity along the same slant angle; and means responsive to said outputs representing aircraft altitude, aircraft slant velocity, and aircraft slant range for calculating and providing an output signal representing aircraft groundspeed.

Claim 17

The system of claim 12 wherein said means for calculating comprises a microprocessor.

Claim 18

The system of claim 12 further comprising display means coupled to said microprocessor and responsive to the output signal representing groundspeed for providing a visual indication of groundspeed.

Claim 19

The system of claim 12 wherein said means for providing a modulating signal comprises means for providing a triangular modulating signal having an upsweep and a downsweep.

Claim 20

The system of claim 15 wherein said means coupled to said second means further includes means for detecting the beat frequency produced during the downsweep of said triangular modulating signal, and means for detecting the beat frequency produced during the upsweep of said triangular modulating signal.

Claim 21

The system of claim 16 wherein said means for calculating includes means for summing the beat frequency produced by said fourth means during the downsweep of said triangular modulating signal with the beat frequency produced by said fourth means during the upsweep of said triangular modulating signal to produce said output representing slant range, and means for subtracting the beat frequency produced by said fourth means on the upsweep of the triangular modulating signal from the beat frequency produced by said fourth means on the downsweep of the triangular modulating signal to produce said output representing slant velocity.

Claim 22

The system of claim 12 wherein said means for calculating further includes means for correcting the calculated groundspeed to compensate for variations in the vertical velocity of an aircraft.

Claim 23

The system of claim 18 wherein said means for calculating further includes means for correcting said groundspeed for variations in the slant angle in order to compensate for the varaitions in the angle of return of the reflected signal from said second target area.

Claim 26

The method of claim 20 wherein said calculating step includes the step of compensating said groundspeed signal for variations in aircraft vertical velocity.

Claim 27

The method of claim 21 wherein said calculating step includes the step of compensating said groundspeed signal for variations in the slant angle of the reflected return signals from said second target area.