Method for monitoring the earth surface
AssigneeDaimler-Benz Aerospace AG
InventorChristoph Neumann
Life of this patent
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Abstract
The invention relates to a method for monitoring the earth's surface with a moving aircraft using a radar sensor with a synthetic aperture. In order to produce high resolution radar images, the flight parameters of the aircraft are also required. According to the inventive method, key parameters, such as speed and acceleration, are detected in the sight line of the radar sensor from the radio signals received. One of the advantages of the invention is that an inertial navigation system (INS) is no longer required for this purpose.
Claims14
A method for monitoring the earth's surface by using an aircraft having a synthetic aperture radar sensor, comprising the steps of:
- (a) using a transmitting/receiving antenna of the radar sensor to illuminate a spot in a region to be monitored, the illuminated spot having a predetermined spatial resolution;
- (b) receiving, radar signals via the transmitting/receiving antenna;
- (c) generating a radar image from the received radar signals through superimposing Fourier spectra, which succeed each other in time and which have been processed block-by-block with respect to a range parameter and a Doppler parameter;
- (d) determining acceleration on a line of sight (Blos) between the illuminated spot and the transmitting/receiving antenna, as well as ambiguity errors on the line of sight (Mlos), step (d) including correlating the Fourier spectra in an azimuth dimension and an elevation dimension;
- (e) determining a speed component on the line of sight (Rlos) within an ambiguity range by estimating an echo center of gravity of the Doppler parameter within the Fourier spectra;
- (f) determining a definite speed on the line of sight (Vlos) in accordance with the following formula:
- (Vlos)=Mlos)·λBm/2+Rlos,
- wherein
- ·=multiplication operator
- λ=radar wave length;
- and
- Bm=measuring band width of the radar sensor in Doppler;
- and
- (g) determining a phase correction “range” parameter (φr) and a phase correction Doppler parameter (φd), which are necessary for focusing radar images, from the acceleration on the line of sight (Blos) and the speed on the line of sight (Vlos).
A method for monitoring the earth's surface by using an aircraft having a synthetic aperture radar sensor, comprising the steps of:
- (a) using a transmitting/receiving antenna of the radar sensor to illuminate a spot in a region to be monitored, the illuminated spot having a predetermined spatial resolution;
- (b) receiving radar signals via the transmitting/receiving antenna;
- (c) generating a radar image from the received radar signals through superimposing Fourier spectra, which succeed each other in time and which have been processed block-by-block with respect to a Doppler parameter;
- (d) determining acceleration on a line of sight (Blos) between the illuminated spot and the transmitting/receiving antenna, as well as ambiguity errors on the line of sight (Mlos), step (d) including correlating the Fourier spectra in an azimuth dimension and an elevation dimension;
- (e) determining a speed component on the line of sight (Rlos) within an ambiguity range by estimating an echo center of gravity of the Doppler parameter within the Fourier spectra;
- (f) determining a definite speed on the line of sight (Vlos) in accordance with the following formula:
- (Vlos)=(Mlos)·λBm/2+Rlos,
- wherein
- ·=multiplication operator
- λ=radar wave length;
- and
- Bm=measuring band width of the radar sensor in Doppler;
- (g) determining a phase correction “range” parameter (φr) and a phase correction Doppler parameter (φd), which are necessary for focusing radar images, from the acceleration on the line of sight (Blos) and the speed on the line of sight (Vlos).
Dependencies are inferred from the claim text.