Claims Analysis
Total Claims: 24
Claim 1
Independent Claim
306 words
A miss distance indicator data processing and recording apparatus for determining and indicating a miss distance for a missile tracking a target comprising: antenna means for receiving a radio frequency missile telemetry signal from said missile and a translated radio frequency missile telemetry signal from said target; first receiver means connected to said antenna means to receive said radio frequency missile telemetry signal, said first receiver means filtering and amplifying said radio frequency missile telemetry signal and then down converting said radio frequency missile telemetry signal to a first predetection carrier signal; second receiver means connected to said antenna means to receive said translated radio frequency missile telemetry signal, said second receiver means filtering and amplifying said translated radio frequency missile telemetry signal and then down converting said translated radio frequency missile telemetry signal to a second predetection carrier signal; mixer means connected to said first receiver means to receive said first predetection carrier signal and said second receiver means to receive said second predetection carrier signal, said mixer means producing a difference frequency signal equal to the frequency difference between said first predetection carrier signal and said second predetection carrier signal; frequency analyzer means connected to said mixer means to receive said difference frequency signal, said frequency analyzer means processing said difference frequency signal to generate a plot of doppler frequency versus time which is used to determine the miss distance said missile misses said target in accordance with the expression: ##EQU7## where Δf is a frequency difference which said frequency analyzer means determines and then displays; Δt is a time difference which said frequency analyzer means determines and then displays and λ is constant for said radio frequency missile telemetry signal; and printer means connected to said frequency analyzer means, said printer means generating a printout of said plot of doppler frequency versus time.
Claim 2
Dependent Claim
306 words
A miss distance indicator data processing and recording apparatus for determining and indicating a miss distance for a missile tracking a target comprising: antenna means for receiving a radio frequency missile telemetry signal from said missile and a translated radio frequency missile telemetry signal from said target; first receiver means connected to said antenna means to receive said radio frequency missile telemetry signal, said first receiver means filtering and amplifying said radio frequency missile telemetry signal and then down converting said radio frequency missile telemetry signal to a first predetection carrier signal; second receiver means connected to said antenna means to receive said translated radio frequency missile telemetry signal, said second receiver means filtering and amplifying said translated radio frequency missile telemetry signal and then down converting said translated radio frequency missile telemetry signal to a second predetection carrier signal; mixer means connected to said first receiver means to receive said first predetection carrier signal and said second receiver means to receive said second predetection carrier signal, said mixer means producing a difference frequency signal equal to the frequency difference between said first predetection carrier signal and said second predetection carrier signal; frequency analyzer means connected to said mixer means to receive said difference frequency signal, said frequency analyzer means processing said difference frequency signal to generate a plot of doppler frequency versus time which is used to determine the miss distance said missile misses said target in accordance with the expression: ##EQU7## where Δf is a frequency difference which said frequency analyzer means determines and then displays; Δt is a time difference which said frequency analyzer means determines and then displays and λ is constant for said radio frequency missile telemetry signal; and printer means connected to said frequency analyzer means, said printer means generating a printout of said plot of doppler frequency versus time.
Claim 3
Dependent Claim
24 words
The miss distance indicator data processing and recording apparatus of claim 1 wherein said first and second receiver means each comprise a telemetry receiver.
Claim 4
Dependent Claim
21 words
The miss distance indicator data processing and recording apparatus of claim 1 wherein said mixer means comprises a double balanced mixer.
Claim 5
Dependent Claim
26 words
The miss distance indicator data processing and recording apparatus of claim 1 wherein said radio frequency missile telemetry signal has a frequency of about 2215.5 Megahertz.
Claim 6
Dependent Claim
27 words
The miss distance indicator data processing and recording apparatus of claim 1 wherein said translated radio frequency missile telemetry signal has a frequency of about 1826 Megahertz.
Claim 7
Dependent Claim
26 words
The miss distance indicator data processing and recording apparatus of claim 1 wherein said constant λ for said radio frequency missile telemetry signal is about 0.444.
Claim 8
Dependent Claim
305 words
A miss distance indicator data processing and recording apparatus for determining and indicating a miss distance for a missile tracking a target comprising: an antenna for receiving a radio frequency missile telemetry signal from said missile and a translated radio frequency missile telemetry signal from said target; a first telemetry receiver connected to said antenna to receive said radio frequency missile telemetry signal, said first telemetry receiver filtering and amplifying said radio frequency missile telemetry signal and then down converting said radio frequency missile telemetry signal to a first predetection carrier signal; a second telemetry receiver connected to said antenna to receive said translated radio frequency missile telemetry signal, said second telemetry receiver filtering and amplifying said translated radio frequency missile telemetry signal and then down converting said translated radio frequency missile telemetry signal to a second predetection carrier signal; a double balanced mixer connected to said first telemetry receiver to receive said first predetection carrier signal and said second telemetry receiver to receive said second predetection carrier signal, said double balanced mixer producing a difference frequency signal equal to the frequency difference between said first predetection carrier signal and said second predetection carrier signal; a frequency analyzer connected to said double balanced mixer to receive said difference frequency signal; said frequency analyzer processing said difference frequency signal to generate a plot of doppler frequency versus time which is used to determine the miss distance said missile misses said target in accordance with the expression: ##EQU8## where Δf is a frequency difference which said frequency analyzer determines and then displays; Δt is a time difference which said frequency analyzer determines and then displays and λ is constant for said radio frequency missile telemetry signal; and a printer connected to said frequency analyzer, said printer generating a printout of said plot of doppler frequency versus time.
Claim 9
Dependent Claim
305 words
A miss distance indicator data processing and recording apparatus for determining and indicating a miss distance for a missile tracking a target comprising: an antenna for receiving a radio frequency missile telemetry signal from said missile and a translated radio frequency missile telemetry signal from said target; a first telemetry receiver connected to said antenna to receive said radio frequency missile telemetry signal, said first telemetry receiver filtering and amplifying said radio frequency missile telemetry signal and then down converting said radio frequency missile telemetry signal to a first predetection carrier signal; a second telemetry receiver connected to said antenna to receive said translated radio frequency missile telemetry signal, said second telemetry receiver filtering and amplifying said translated radio frequency missile telemetry signal and then down converting said translated radio frequency missile telemetry signal to a second predetection carrier signal; a double balanced mixer connected to said first telemetry receiver to receive said first predetection carrier signal and said second telemetry receiver to receive said second predetection carrier signal, said double balanced mixer producing a difference frequency signal equal to the frequency difference between said first predetection carrier signal and said second predetection carrier signal; a frequency analyzer connected to said double balanced mixer to receive said difference frequency signal; said frequency analyzer processing said difference frequency signal to generate a plot of doppler frequency versus time which is used to determine the miss distance said missile misses said target in accordance with the expression: ##EQU8## where Δf is a frequency difference which said frequency analyzer determines and then displays; Δt is a time difference which said frequency analyzer determines and then displays and λ is constant for said radio frequency missile telemetry signal; and a printer connected to said frequency analyzer, said printer generating a printout of said plot of doppler frequency versus time.
Claim 10
Dependent Claim
26 words
The miss distance indicator data processing and recording apparatus of claim 7 wherein said radio frequency missile telemetry signal has a frequency of about 2215.5 Megahertz.
Claim 11
Dependent Claim
27 words
The miss distance indicator data processing and recording apparatus of claim 7 wherein said translated radio frequency missile telemetry signal has a frequency of about 1826 Megahertz.
Claim 12
Dependent Claim
25 words
The miss distance indicator data processing and recording apparatus of claim 7 wherein said first predetection carrier signal has a frequency of about 900 kilohertz.
Claim 13
Dependent Claim
25 words
The miss distance indicator data processing and recording apparatus of claim 7 wherein said second predetection carrier signal has a frequency of about 924 kilohertz.
Claim 14
Dependent Claim
26 words
The miss distance indicator data processing and recording apparatus of claim 7 wherein said constant λ for said radio frequency missile telemetry signal is about 0.444.
Claim 15
Dependent Claim
346 words
A miss distance indicator data processing and recording apparatus for determining and indicating a miss distance for a missile tracking a target comprising: an antenna for receiving a radio frequency missile telemetry signal from said missile and a translated radio frequency missile telemetry signal from said target; a first telemetry receiver connected to said antenna to receive said radio frequency missile telemetry signal, said first telemetry receiver filtering and amplifying said radio frequency missile telemetry signal and then down converting said radio frequency missile telemetry signal to a first predetection carrier signal; a second telemetry receiver connected to said antenna to receive said translated radio frequency missile telemetry signal, said second telemetry receiver filtering and amplifying said translated radio frequency missile telemetry signal and then down converting said radio frequency missile telemetry signal to a second predetermined carrier signal; an analog magnetic tape recorder connected to said first telemetry receiver to receive said first predetection carrier signal and said second telemetry receiver to receive said second predetection carrier signal, said analog magnetic tape recorder recording said first predetection carrier signal and said second predetection carrier signal; a double balanced mixer connected to said analog magnetic tape recorder to receive said first predetection carrier signal and said second predetection carrier signal, said double balanced mixer producing a difference frequency signal equal to the frequency difference between said first predetection carrier signal and said second predetection carrier signal; a frequency analyzer connected to said double balanced mixer to receive said difference frequency signal; said frequency analyzer processing said difference frequency signal to generate a plot of doppler frequency versus time which is used to determine the miss distance said missile misses said target in accordance with the expression: ##EQU9## where Δf is a frequency difference which said frequency analyzer determines and then displays; Δt is a time difference which said frequency analyzer determines and then displays and λ is constant for said radio frequency missile telemetry signal; and a printer connected to said frequency analyzer, said printer generating a printout of said plot of doppler frequency versus time.
Claim 16
Dependent Claim
346 words
A miss distance indicator data processing and recording apparatus for determining and indicating a miss distance for a missile tracking a target comprising: an antenna for receiving a radio frequency missile telemetry signal from said missile and a translated radio frequency missile telemetry signal from said target; a first telemetry receiver connected to said antenna to receive said radio frequency missile telemetry signal, said first telemetry receiver filtering and amplifying said radio frequency missile telemetry signal and then down converting said radio frequency missile telemetry signal to a first predetection carrier signal; a second telemetry receiver connected to said antenna to receive said translated radio frequency missile telemetry signal, said second telemetry receiver filtering and amplifying said translated radio frequency missile telemetry signal and then down converting said radio frequency missile telemetry signal to a second predetermined carrier signal; an analog magnetic tape recorder connected to said first telemetry receiver to receive said first predetection carrier signal and said second telemetry receiver to receive said second predetection carrier signal, said analog magnetic tape recorder recording said first predetection carrier signal and said second predetection carrier signal; a double balanced mixer connected to said analog magnetic tape recorder to receive said first predetection carrier signal and said second predetection carrier signal, said double balanced mixer producing a difference frequency signal equal to the frequency difference between said first predetection carrier signal and said second predetection carrier signal; a frequency analyzer connected to said double balanced mixer to receive said difference frequency signal; said frequency analyzer processing said difference frequency signal to generate a plot of doppler frequency versus time which is used to determine the miss distance said missile misses said target in accordance with the expression: ##EQU9## where Δf is a frequency difference which said frequency analyzer determines and then displays; Δt is a time difference which said frequency analyzer determines and then displays and λ is constant for said radio frequency missile telemetry signal; and a printer connected to said frequency analyzer, said printer generating a printout of said plot of doppler frequency versus time.
Claim 17
Dependent Claim
26 words
The miss distance indicator data processing and recording apparatus of claim 13 wherein said radio frequency missile telemetry signal has a frequency of about 2215.5 Megahertz.
Claim 18
Dependent Claim
26 words
The miss distance indicator data processing and recording apparatus of claim 13 wherein said radio frequency target telemetry signal has a frequency of about 1826 Megahertz.
Claim 19
Dependent Claim
25 words
The miss distance indicator data processing and recording apparatus of claim 13 wherein said first intermediate frequency signal has a frequency of about 900 kilohertz.
Claim 20
Dependent Claim
25 words
The miss distance indicator data processing and recording apparatus of claim 13 wherein said second intermediate frequency signal has a frequency of about 924 kilohertz.
Claim 21
Dependent Claim
26 words
The miss distance indicator data processing and recording apparatus of claim 13 wherein said constant λ for said radio frequency missile telemetry signal is about 0.444.
Claim 22
Dependent Claim
71 words
The miss distance indicator data processing and recording apparatus of claim 13 further comprising a time code generator connected to said analog magnetic tape recorder, said time code generator receiving externally generated position data, said time code generator extracting time data from said position data, said time code generator providing said time data to said analog magnetic tape recorder, said time code generator having a position data receiving antenna connected thereto.
Claim 23
Independent Claim
209 words
A method for determining a miss distance for a missile tracking a target, comprising the steps of: at a receiving location, receiving a radio frequency missile telemetry signal from said missile and a translated radio frequency missile telemetry signal from said target; filtering and amplifying said radio frequency missile telemetry signal; down converting said radio frequency missile telemetry signal to a first predetection carrier signal; filtering and amplifying said translated radio frequency missile telemetry signal; down converting said translated radio frequency missile telemetry signal to a second predetection carrier signal; combining said first predetection carrier signal and said second predetection carrier signal to produce a difference frequency signal equal to the frequency difference between said first predetection carrier signal and said second predetection carrier signal; at said receiving location, receiving global position system data, said global position system data including time data; extracting said time data from said global position system data; processing said difference frequency signal to generate a plot of doppler frequency versus time which is used to determine the miss distance said missile misses said target; processing said time data to determine an exact time when said missile misses said target at said miss distance; generating a printout of said plot of doppler frequency versus time.
Claim 24
Independent Claim
209 words
A method for determining a miss distance for a missile tracking a target, comprising the steps of: at a receiving location, receiving a radio frequency missile telemetry signal from said missile and a translated radio frequency missile telemetry signal from said target; filtering and amplifying said radio frequency missile telemetry signal; down converting said radio frequency missile telemetry signal to a first predetection carrier signal; filtering and amplifying said translated radio frequency missile telemetry signal; down converting said translated radio frequency missile telemetry signal to a second predetection carrier signal; combining said first predetection carrier signal and said second predetection carrier signal to produce a difference frequency signal equal to the frequency difference between said first predetection carrier signal and said second predetection carrier signal; at said receiving location, receiving global position system data, said global position system data including time data; extracting said time data from said global position system data; processing said difference frequency signal to generate a plot of doppler frequency versus time which is used to determine the miss distance said missile misses said target; processing said time data to determine an exact time when said missile misses said target at said miss distance; generating a printout of said plot of doppler frequency versus time.