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US3937945A Expired / Lapsed US ⏱️ 0.0 years remaining

Apparatus for simulating optical transmission links

Assignee: National Aeronautics and Space Administration
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Filing: 1974-06-25
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Granted: 1976-02-10
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Expires: 1994-06-25
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Abstract

Abstract A space-to-space or space-to-earth optical transmission link is simulated by positioning a linear optical modulator between an optical carrier source and a receiver for the carrier. The optical modulator is driven by an analog signal having random variations indicative of characteristics of the transmission link, as derived from an analog computer circuit. The analog computer circuit is responsive to a Gaussian random analog source. For certain types of links, the analog computer circuit is responsive to a pair of Gaussian analog signals which are derived by feeding a relatively wide band Gaussian analog source in parallel to a first low pass filter and to a heterodyne circuit that derives a beat frequency output that is passed through a second low pass filter having the same characteristics as the first low pass filter. For space-to-space transmission, transmitter pointing jitter is a dominant noise source and is simulated by deriving a beta statistical variation from the analog computer. For space-to-earth transmission, atmospheric scintillation is a dominant noise source and is simulated by driving the modulator with one of (1) a log normal, (2) Rayleigh, or (3) Ricean output of the analog computer circuit.

Inventors

  • 👤 Michael W. Fitzmaurice
  • 👤 Mona Tycz

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 22:35
CPC Classifications
H; H04; H04B; H04B10/00; H04B10/50; H04B10/501; H04B10/503; H04B10/505

Claims Analysis

Total Claims: 14
Claim 1
Independent Claim 88 words
Apparatus for simulating a space-to-space or space-to-earth optical transmission link comprising a Gaussian random source, a computer responsive to the Gaussian random source for deriving an analog signal having random variations indicative of characteristics of the transmission link, and a linear optical modulator connected to be responsive to the analog signal and adapted to be positioned between an optical carrier source and a receiver for the carrier of the source, whereby light transmitted through the modulator is modulated in accordance with the random variations of the analog signal.
Claim 2
Dependent Claim 88 words
Apparatus for simulating a space-to-space or space-to-earth optical transmission link comprising a Gaussian random source, a computer responsive to the Gaussian random source for deriving an analog signal having random variations indicative of characteristics of the transmission link, and a linear optical modulator connected to be responsive to the analog signal and adapted to be positioned between an optical carrier source and a receiver for the carrier of the source, whereby light transmitted through the modulator is modulated in accordance with the random variations of the analog signal.
Claim 3
Dependent Claim 79 words
The apparatus of claim 1 wherein the Gaussian source includes means for deriving first and second random Gaussian signals having a substantially zero cross-correlation coefficient, said computer including: means responsive to the first and second signals for deriving a third signal having a magnitude commensurate with the value of the sum of the squares of the first and second signals, and means responsive to the third signal for deriving the analog signal as a function of the third signal.
Claim 4
Dependent Claim 52 words
The apparatus of claim 2 wherein the means for deriving the third signal includes antilog converter means responsive to the third signal for deriving the analog signal as a beta output for modulating the optical energy coupled through the modulator to simulate a space-to-space optical transmission link having pointing errors imposed thereon.
Claim 5
Dependent Claim 47 words
The apparatus of claim 2 wherein the deriving means includes means for applying a replica of variations of the third signal to the modulator as a chi-squared output for amplitude modulating the light coupled through the modulator to simulate a space-to-earth optical transmission link having atmospheric perturbations.
Claim 6
Dependent Claim 40 words
The apparatus of claim 4 further including means for selectively offsetting one of the Gaussian random signals, whereby the chi-squared output respectively simulates Ricean and Rayleigh modulation while the offset is and is not imposed on the one Gaussian signal.
Claim 7
Dependent Claim 105 words
The apparatus of claim 2 wherein the means for deriving the first and second Gaussian signals includes an analog Gaussian signal source having at least a first predetermined bandwidth, bandpass filter means responsive to only a first segment of th bandwidth of the analog Gaussian source for deriving the first signal as an additional analog signal having a second predetermined bandwidth less than the first bandwidth, and heterodyne means responsive to only a second segment of the bandwidth of the analog Gaussian source for deriving the second signal as a further analog signal having the same bandwidth as the bandwidth of the additional analog signal.
Claim 8
Dependent Claim 58 words
The apparatus of claim 6 wherein the means for deriving the additional signal includes low pass filter means for deriving the additional signal as a baseband signal, and the means for deriving the further signal includes low pass filter means responsive to a beat frequency of the heterodyne means for deriving the further signal as a baseband signal.
Claim 9
Dependent Claim 29 words
The apparatus of claim 1 wherein the computer includes antilog converter means for deriving the analog signal as a function of the antilog of variations of the Gaussian source.
Claim 10
Dependent Claim 77 words
The apparatus of claim 8 wherein the computer includes means for offsetting the variations of the Gaussian source, and means for coupling the offset variations to the antilog converter means, and means for coupling a replica of variations of the antilog converter to the modulator as the analog signal to modulate optical energy coupled through the modulator, whereby the irradiance output of the modulator simulates log normal characteristics of a space-to-earth transmission link due to atmospheric perturbations.
Claim 11
Dependent Claim 57 words
The apparatus of claim 1 wherein Rayleigh amplitude modulation can be simulated, said Gaussian random source includes a means for deriving first and second analog signals having a substantially zero cross correlation coefficient, and said computer is responsive to the first and second analog signals for deriving an analog signal having variations proportional to Rayleigh amplitude modulation.
Claim 12
Dependent Claim 57 words
The apparatus of claim 1 wherein Ricean amplitude modulation can be simulated, said Gaussian random source includes a means for deriving first and second analog signals having a substantially zero cross correlation coefficient, and said computer is responsive to the first and second analog signals for deriving an analog signal having variations proportional to Ricean amplitude modulation.
Claim 13
Dependent Claim 57 words
The apparatus of claim 1 where beta irradiance modulation can be simulated, said Gaussian random source includes a means for deriving first and second analog signals having a substantially zero cross correlation coefficient, and said computer is responsive to the first and second analog signals for deriving an analog signal having variations proportional to beta irradiance modulation.
Claim 14
Dependent Claim 59 words
The apparatus of claim 1 wherein log normal irradiance modulation can be simulated, said Gaussian random source includes a means for deriving first and second analog signals having a substantially zero cross correlation coefficient and said computer is responsive to the first and second analog signals for deriving an analog signal having varations proportional to log normal irradiance modulation.

References Cited (Backward Citations)

US3124678A Cited
US3243592A Cited
US3752992A Cited
US3714437A Cited
US3787118A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1979-02-09 1979-08-11 1980-02-10 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1983-02-09 1983-08-11 1984-02-10 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1987-02-09 1987-08-11 1988-02-10 $7700.00 Window Closed / Lapsed

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