Automated aircraft radio navigation simulator

Claim 2

Apparatus for automatically simulating the glideslope, localizer and very high frequency, omnidirection (VOR) guidance signals received by an aircraft comprising control means for producing digital signals representative of: a) a desired final glideslope value and the rate which said final glideslope value should be approached, b) a desired final localizer value and the rate at which said final localizer value should be approached, c) a desired final VOR value and the rate at which said final VOR value should be approached; glideslope circuitry means including means to receive the digital signals representative of the final glideslope value and the rate at which said final glideslope value should be approached and means responsive to said received signals to generate said desired final value at said desired rate; localizer circuitry means including means to receive the digital signals representative of the final localizer value and the rate at which said final localizer value should be approached and means responsive to said received signals to generate said desired final value at said desired rate; and VOR circuitry means including means to receive the digital signals representative of the final VOR value and the rate at said final VOR value should be approached and means responsive to said received signals to generate said desired final value at said desired rate.

Claim 3

The apparatus of claim 1 wherein the control means is connected to the glideslope circuitry means, localizer circuitry means and VOR circuitry means on a common bus and wherein each of said glideslope, localizer and VOR circuitry is assigned a unique digital address, which address is known by the control means, such that a selected one of the glideslope, localizer and VOR circuitry means responds to data on the bus in accordance with its address being present therewith.

Claim 5

The apparatus of claim 3 wherein the logic means comprises: counter means for storing the instantaneous value of said glideslope signal therein, said counter means being actuable to incrementally up or down count its stored value; and comparator means for comparing said instantaneous glideslope signal, as stored in said counter means, with the desired final value, as stored in said final value register means, and, should said values differ, actuating said counter means, at the rate determined by said rate signal as stored in said rate register means, to incrementally count up or down such that said instantaneous value increments towards the desired value.

Claim 6

The apparatus of claim 3 wherein said logic means further comprises: a fixed frequency rate oscillator producing a fixed frequency rate signal f r ; divider means for dividing said signal f r by a divisor N producing a signal of frequency f r /N, said divisor N being determined by the rate signal stored in the rate register means; and means coupling said signal f r /N to said counter means to control the rate of incrementing thereof.

Claim 7

The apparatus of claim 3 wherein said combiner means comprises: means for producing a signal (K-V c ) equal to the difference between said constant level K and the value of said control signal V ; first multiplier means for multiplying said generated fixed level signal f 1 by the level of said control signal V ; second multiplier means for multiplying said generated fixed level signal f 2 by said signal (K-V c ); and means for summing the outputs of the first and second multipliers.

Claim 9

The apparatus of claim 7 wherein the logic means comprises: counter means for storing the instantaneous value of said localizer signal therein, said counter means being actuable to incrementally up or down count its stored value: and comparator means for comparing said instantaneous localizer signal, as stored in said counter means, with the desired final value, as stored in said final value register means, and, should said values differ, actuating said counter means, at the rate determined by said rate signal as stored in said rate register means, to incrementally count up or down such that said instantaneous value increments towards the desired value.

Claim 10

The apparatus of claim 7 wherein said logic means further comprises: a fixed frequency rate oscillator producing a fixed frequency rate signal f r ; divider means for dividing said signal f r by a divisor N producing a signal frequency f r/ N, said divisor N being determined by the rate signal stored in the rate register means; and means coupling said signal f r/ N to said counter means to control the rate of incrementing thereof.

Claim 11

The apparatus of claim 7 wherein said combiner means comprises: means for producing a signal (K-V ) equal to the difference between said constant level K and the value of said control signal V c ; first multiplier means for multiplying said generated fixed level signal f 1 by the level of said control signal V c ; second multiplier means for multiplying said generated ifxed level signal f 2 by said signal (K-Vc); and means for summing the outputs of the first and second multipliers.

Claim 13

The apparatus of claim 11 wherein the logic means comprises; counter means for storing the instantaneous value of said VOR signal therein, said counter means being actuable to incrementally up or down count its stored value; and comparator means for comparing said instantaneous VOR signal, as stored in said counter means, with the desired final value, as stored in said final value register means, and, should said values differ, actuating said counter means, at the rate determined by said rate signal as stored in said rate register means, to incrementally count up or down such that said instantaneous value increments towards the desired value.

Claim 14

The apparatus of claim 12 wherein said logic means further comprises: a fixed frequency rate oscillator producing a fixed frequency rate signal f ; divider means for dividing said signal f r by a divisor N producing a signal of frequency f r/ N, said divisor being determined by the rate signal stored in the rate register means; and means for coupling said signal f r/ N to said counter means to control the rate of incrementing thereof.

Claim 15

The apparatus of claim 11 further having the capability of automatically simulating aircraft marker beacon tones, each of said tones being representative of the distance of said aircraft from a reference site, the apparatus further comprising: the control means including means for generating a digital signal representative of a desired marker beacon tone; a marker beacon tone register means for storing said marker beacon tone therein; and means for coupling said stored marker beacon tone signal to said generator means causing said generator to produce the desired tone.

Claim 16

1 5. Apparatus for automatically simulating an aircraft glideslope or localizer signal, said signal being comprised of the combination of a first signal f of a first frequency and a second signal f 2 of a second frequency, with the sum of the amplitudes of said signals being a constant level K, the apparatus comprising: control means for generating digital signals representative of the desired final value of the amplitudes of the signals f l and f 2 and the rate at which said final value should be approached; final value register means for receiving and retaining said final value signal; rate register means for receiving and retaining said rate signal; logic means for retaining the present value of said glideslope or localizer signal and digitally incrementing, at the rate determined by said rate register retained signal, to said final value as stored in said final value register; digital to analog converter means for converting said logic means present value, incremental values and final value digital signals to corresponding analog control levels having an instantaneous value of V ; means for generator fixed levels of said signals f 1 and f2; and combiner means, being responsive to said analog control level V c , for processing said generated signals f and f 2 such that the amplitude of each is a predetermined function of said control signal V and the combined amplitude of said signals f 1 and f 2 is said constant level K.

Claim 17

1 5. Apparatus for automatically simulating an aircraft glideslope or localizer signal, said signal being comprised of the combination of a first signal f of a first frequency and a second signal f 2 of a second frequency, with the sum of the amplitudes of said signals being a constant level K, the apparatus comprising: control means for generating digital signals representative of the desired final value of the amplitudes of the signals f l and f 2 and the rate at which said final value should be approached; final value register means for receiving and retaining said final value signal; rate register means for receiving and retaining said rate signal; logic means for retaining the present value of said glideslope or localizer signal and digitally incrementing, at the rate determined by said rate register retained signal, to said final value as stored in said final value register; digital to analog converter means for converting said logic means present value, incremental values and final value digital signals to corresponding analog control levels having an instantaneous value of V ; means for generator fixed levels of said signals f 1 and f2; and combiner means, being responsive to said analog control level V c , for processing said generated signals f and f 2 such that the amplitude of each is a predetermined function of said control signal V and the combined amplitude of said signals f 1 and f 2 is said constant level K.

Claim 18

The apparatus of claim 15 wherein the logic means comprises: counter means for storing the instantaneous value of said glideslope or localizer signal therein, said counter means being actuable to incrementally up or down count its stored value; and comparator means for comparing said instantaneous glideslope or localizer signal, as stored in said counter means, with the desired final value, as stored in said final value register means, and, should said values differ, actuating said counter means, at the rate determined by said rate signal as stored in said rate register means, to incrementally count up or down such that said instantaneous value increments towards the desired value.

Claim 19

The apparatus of claim 16 wherein said logic means further comprises: a fixed frequency rate oscillator producing a fixed frequency rate signal f r ; divider means for dividing said signal f r by a divisor N producing a signal of frequency f r/ N, said divisor N being determined by the rate signal stored in the rate register means; and means coupling said signal f r /N to said counter means to control the rate of incrementing thereof.

Claim 20

The apparatus of claim 15 wherein said combiner means comprises: means for producing a signal (K-V ) equal to the difference between said constant level K and the value of said control signal V ; first multiplier means for multiplying said generated fixed level signal f 1 by the level of said control signal V ; second multiplier means for multiplying said generated fixed level signal f 2 by said signal (K-V c ); and means for summing the outputs of the first and second multipliers.

Claim 21

Apparatus for automatically simulating an aircraft very high frequency, omnidirectional (VOR) guidance path signal comprising: control means for generating digital signals representative of the desired final value VOR signal and of the rate at which said final value should be approached; final value register means for receiving and retaining said final value signal; rate register means for receiving and retaining said rate signal; logic means for retaining the present value of said VOR signal and digitally incrementing, at the rate determined by said rate register retained signal, to said final value as stored in said final value register; switching means for activating predetermined switches in response to the status of said logic means; and generator means responsive to the status of said switching means for generating a predetermined VO R signal in response thereto.

Claim 22

Apparatus for automatically simulating an aircraft very high frequency, omnidirectional (VOR) guidance path signal comprising: control means for generating digital signals representative of the desired final value VOR signal and of the rate at which said final value should be approached; final value register means for receiving and retaining said final value signal; rate register means for receiving and retaining said rate signal; logic means for retaining the present value of said VOR signal and digitally incrementing, at the rate determined by said rate register retained signal, to said final value as stored in said final value register; switching means for activating predetermined switches in response to the status of said logic means; and generator means responsive to the status of said switching means for generating a predetermined VO R signal in response thereto.

Claim 23

The apparatus of claim 19 wherein the logic means comprises: counter means for storing the instantaneous value of said VOR signal therein, said counter means being actuable to incrementally up or down count its stored value; comparator means for comparing said instantaneous VOR signal, as stored in said counter means, with the desired final value, as stored in said final value register means, and, should said values differ, actuating said counter means, at the rate determined by said rate signal as stored in said rate register means, to incrementally count up or down such that said instantaneous value increments toward the desired value.

Claim 24

The apparatus of claim 20 wherein said logic means further comprises: a fixed frequency rate oscillator producing a fixed frequency rate signal f ; divider means for dividing said signal f by a divisor N producing a signal of frequency f r /N, said divisor N being determined by the rate signal stored in the rate register means; and means coupling said signal f r/ N to said counter means to control the rate of incrementing thereof.

Claim 25

The apparatus of claim 14 further having the capability of automatically simulating aircraft markter beacon tones, each of said tones being representative of the distance of said aircraft from a reference site, the apparatus further comprising: the control means including means for generating a digital signal representative of a desired marker beacon tone; a marker beacon tone register means for storing said marker beacon tone therein; and means for coupling said stored marker beacon tone signal to said generator means causing said generator to produce the desired tone.