Patent US4908785A successfully refreshed from Google Patents.
US4908785A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Data compression method for telemetry of vibration data
Assignee: Boeing Co
•
Filing: 1985-08-16
•
Granted: 1990-03-13
•
Expires: 2005-08-16
Abstract
Abstract Vibrational data is compressed about 8.5 to 18 times by isolating a low frequency component from the signal, frequency analyzing the signal to obtain important frequency/amplitude data, and recombining the low frequency component with the analyzed information for efficient transmission.
Inventors
- 👤 Thomas D. Cubbins
- 👤 Thomas R. Hope
- 👤 John M. Michels
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-03 14:30
CPC Classifications
H; H04; H04B; H04B1/00; H04B1/66; H04B1/667
Claims Analysis
Total Claims: 21
Claim 1
Independent Claim
148 words
A method for compressing vibration data for telemetry from a missile or spacecraft while allowing complete assessment of important vibration modes, comprising the steps of: (a) sensing the missile vibration at a predetermined sample rate with at least one strain gauge to generate raw vibration data; (b) splitting the signal into a first and a second signal path, the paths being electrically connected in parallel; (c) filtering the raw vibration data in the first signal path to obtain an uncompressed low frequency component suitable for transmission; (d) frequency analyzing the data in the second signal path into compressed frequency/amplitude data suitable to identify sources of high frequency vibrations; and (e) multiplexing the compressed frequency/ amplitude data with the low frequency component without further signal processing of either component to provide a mixed signal, the mixed signal being compressed from the raw signal and being suitable for efficient transmission.
Claim 2
Independent Claim
148 words
A method for compressing vibration data for telemetry from a missile or spacecraft while allowing complete assessment of important vibration modes, comprising the steps of: (a) sensing the missile vibration at a predetermined sample rate with at least one strain gauge to generate raw vibration data; (b) splitting the signal into a first and a second signal path, the paths being electrically connected in parallel; (c) filtering the raw vibration data in the first signal path to obtain an uncompressed low frequency component suitable for transmission; (d) frequency analyzing the data in the second signal path into compressed frequency/amplitude data suitable to identify sources of high frequency vibrations; and (e) multiplexing the compressed frequency/ amplitude data with the low frequency component without further signal processing of either component to provide a mixed signal, the mixed signal being compressed from the raw signal and being suitable for efficient transmission.
Claim 3
Dependent Claim
23 words
The method of claim 1 wherein the frequency analysis includes parallel bank filtering of the raw signal to enhance the speed of analysis.
Claim 4
Dependent Claim
18 words
The method of claim 1 wherein the frequency analysis includes isolating frequency/amplitude data on a 1/3 octave basis.
Claim 5
Dependent Claim
16 words
The method of claim 1 wherein the low frequency--high frequency split is at about 600 Hz.
Claim 6
Dependent Claim
14 words
The method of claim 1 wherein the data sample rate is about 20,000 samples/sec.
Claim 7
Dependent Claim
19 words
The method of claim 1 wherein the frequency analysis includes isolating frequency amplitude data on a 1/6 octave basis.
Claim 8
Dependent Claim
44 words
The method of claim 1 wherein the vibration data has a bandwidth of about 0-10,000 Hz, the uncompressed low frequency component has a maximum frequency of about 600 Hz, the sample rate is about 20,000 samples/sec, and the compression ratio is between about 8.5-18.0.
Claim 9
Dependent Claim
15 words
The method of claim 7 wherein the spectral analysis uses Fast Fourier Transform spectral analysis.
Claim 10
Dependent Claim
14 words
The method of claim 1 wherein the frequency analysis includes Fourier Transform spectral analysis.
Claim 11
Dependent Claim
11 words
The method of claim 9 wherein the spectral analysis uses DFT.
Claim 12
Dependent Claim
11 words
The method of claim 9 wherein the spectral analysis uses FFT.
Claim 13
Dependent Claim
144 words
A telemetry data compression system for compressing vibration data generated on a missile or spacecraft, comprising: (a) means for sensing the vibration and for creating a vibration signal at a predetermined sample rate; (b) means for splitting the vibration signal into a first and second signal path, the paths being electrically connected in parallel; (c) a filter along the first path to isolate a low frequency component from the vibration signal; (d) a frequency spectral analyzer along the second path for analyzing the parallel vibrational signal into an analyzed component having frequency/amplitude bands across the signal bandwidth, the bands being representative of the important vibrational modes contained within the signal; and (e) a multiplexer connected to the filter and the analyzer for combining the low frequency component with the analyzed component for transmission of the compressed data without further signal processing of either component.
Claim 14
Dependent Claim
144 words
A telemetry data compression system for compressing vibration data generated on a missile or spacecraft, comprising: (a) means for sensing the vibration and for creating a vibration signal at a predetermined sample rate; (b) means for splitting the vibration signal into a first and second signal path, the paths being electrically connected in parallel; (c) a filter along the first path to isolate a low frequency component from the vibration signal; (d) a frequency spectral analyzer along the second path for analyzing the parallel vibrational signal into an analyzed component having frequency/amplitude bands across the signal bandwidth, the bands being representative of the important vibrational modes contained within the signal; and (e) a multiplexer connected to the filter and the analyzer for combining the low frequency component with the analyzed component for transmission of the compressed data without further signal processing of either component.
Claim 15
Dependent Claim
15 words
The system of claim 12 wherein the frequency spectral analyzer performs DFT Fourier Transform analysis.
Claim 16
Dependent Claim
21 words
The system of claim 12 wherein the filter isolates a low frequency component having a maximum frequency of about 600 Hz.
Claim 17
Dependent Claim
17 words
The system of claim 12 wherein the sample rate for the vibrational signal is about 20,000 samples/sec.
Claim 18
Dependent Claim
15 words
The system of claim 12 wherein the frequency spectral analyzer preforms FFT Fourier Transform analysis.
Claim 19
Dependent Claim
43 words
The system of claim 12 wherein the frequency spectral analyzer includes means for analyzing the signal using Fourier Transform analysis, wherein the filter isolates a low frequency component having a maximum frequency of 600 Hz, and the sample rate is about 20,000 samples/sec.
Claim 20
Dependent Claim
64 words
The system of claim 12 wherein the means for sensing has a bandwidth of about 0-10,000 Hz, the sample rate is about 20,000 samples/sec, the low frequency component has a maximum frequency of about 600 Hz, the analyzer uses a method selected from the group consisting of parallel bank filtering, Discrete Fourier Transform analysis, or Fast Fourier Transform analysis to prepare the analyzed component.
Claim 21
Dependent Claim
28 words
The system of claim 18 wherein the means for sensing includes at least one strain gauge, and wherein the system achieves a compression ratio of between about 8.5-18.0.
References Cited (Backward Citations)
US31750A
Cited
US2763840A
Cited
US3462555A
Cited
US3471648A
Cited
US3620069A
Cited
US3641550A
Cited
US3742395A
Cited
US4553213A
Cited
US3758758A
Cited
US3959592A
Cited
US3936611A
Cited
US4081749A
Cited
US4157457A
Cited
USRE31750E
Cited
US4408285A
Cited
US4480480A
Cited
US4488240A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1993-03-12 | 1993-09-11 | 1994-03-13 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1997-03-12 | 1997-09-11 | 1998-03-13 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2001-03-12 | 2001-09-11 | 2002-03-13 | $7700.00 | Window Closed / Lapsed |