US5045855A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method for extracting motion errors of a platform carrying a coherent imaging radar system from the raw radar data and device for executing the method
Assignee: Deutsches Zentrum für Luft- und Raumfahrt eV
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Filing: 1990-07-06
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Granted: 1991-09-03
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Expires: 2010-07-06
Abstract
Abstract In a method for extracting motion errors of a platform carrying a coherent imaging radar system from raw radar data, azimuth spectra continuously following each other in time are formed over a set period of time for the imaging of terrains with mainly homogeneous ground reflectivities. An estimate of the ground reflectivity part is performed with a Kalman filter and with the aid of the azimuth spectra represented and system parameters entered. Then the antenna pattern part is obtained by dividing the azimuth spectrum by the estimated ground reflectivity part. By frequency filtering a separation of the drift angle φ(t) from the velocity V b (t) in the LOS- direction of the antenna is subsequently performed and then the velocity obtained is subjected to normalization after having been integrated, from which results the displacement in the line of sight direction of the antenna.
Inventors
- 👤 Joao Moreira
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-07 19:53
CPC Classifications
G; G01; G01S; G01S13/00; G01S13/88; G01S13/89; G01S13/90; G01S13/9004; G01S13/9011
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
222 words
A method for the extraction of motion errors of a platform carrying a coherent imaging radar system from raw radar data, for imaging terrains with mainly homogenous ground reflectivities comprising the steps of: forming azimuth spectra continuously successive in time over a set period of time; estimating, using a prediction filter, a ground reflectivity part of the azimuth spectra from the formed azimuth spectra and entered system parameters as platform's forward velocity, radar range delay, and radar pulse repetition frequency; dividing the azimuth spectrum by said estimated ground reflectivity part to obtain an antenna pattern part of the azimuth spectra; determining a doppler centroid of the antenna pattern part; separating the drift angle part 2 V v (t)sin(φ(t)/λ) of the doppler centroid signal by low pass filtering the doppler centroid signal and a subsequent normalization using the equation arc sin (low-pass-filter-output * λ/2 V.sub.v (t)), in order to obtain the drift angle φ(t), where V v (t) is the platform's forward velocity and λ the wavelength of the transmitted radar signal; and separating the velocity in line of sight direction part (2 V b (t)/λ) of the doppler centroid signal by high pass filtering the doppler centroid signal, in order to obtain the motion errors (displacement) in line of sight direction of the antenna after an integration and subsequent normalization with (λ/2).
Claim 2
Independent Claim
222 words
A method for the extraction of motion errors of a platform carrying a coherent imaging radar system from raw radar data, for imaging terrains with mainly homogenous ground reflectivities comprising the steps of: forming azimuth spectra continuously successive in time over a set period of time; estimating, using a prediction filter, a ground reflectivity part of the azimuth spectra from the formed azimuth spectra and entered system parameters as platform's forward velocity, radar range delay, and radar pulse repetition frequency; dividing the azimuth spectrum by said estimated ground reflectivity part to obtain an antenna pattern part of the azimuth spectra; determining a doppler centroid of the antenna pattern part; separating the drift angle part 2 V v (t)sin(φ(t)/λ) of the doppler centroid signal by low pass filtering the doppler centroid signal and a subsequent normalization using the equation arc sin (low-pass-filter-output * λ/2 V.sub.v (t)), in order to obtain the drift angle φ(t), where V v (t) is the platform's forward velocity and λ the wavelength of the transmitted radar signal; and separating the velocity in line of sight direction part (2 V b (t)/λ) of the doppler centroid signal by high pass filtering the doppler centroid signal, in order to obtain the motion errors (displacement) in line of sight direction of the antenna after an integration and subsequent normalization with (λ/2).
Claim 3
Dependent Claim
163 words
A device for executing the method in accordance with claim 1, comprising an azimuth detection device (400), for the formation of azimuth spectra continuously following each other in time; a prediction filter (401) for estimating the ground reflectivity part; a dividing unit (402) for forming the antenna pattern part; a device (403) for determining the doppler centroid of the antenna pattern part; a high-pass filter (404) for determining the term (2 V b (t)/λ), said high-pass filter being connected with the device for determining the doppler centroid of the antenna pattern part, downstream of which high-pass filter an integrating unit (405) and a normalization unit (406) have been placed for the determination of the displacement in the line of sight direction of the antenna; and a low-pass filter (407) also connected with said device for determining the doppler centroid of the antenna pattern part, downstream of which low-pass filter a normalization unit (408) for the determination of the drift angle (φ(t) is placed.
Claim 4
Dependent Claim
13 words
The method of claim 1, wherein said prediction filter is a Kalman filter.
Claim 5
Dependent Claim
13 words
The device of claim 2, wherein said prediction filter is a Kalman filter.
References Cited (Backward Citations)
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| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
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| 3.5 Years (Year 4) | 1994-09-02 | 1995-03-04 | 1995-09-03 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1998-09-02 | 1999-03-04 | 1999-09-03 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2002-09-02 | 2003-03-04 | 2003-09-03 | $7700.00 | Window Closed / Lapsed |