초록 ▼

A pulse radar device which can sweep in the azimuth direction with a two element direction finding antenna (1, 2) having a fan pattern and wherein the path differences and Doppler frequencies are ranged selective to determine at each azimuth from the echo signals received a mean aspect angle (ε) and

A pulse radar device which can sweep in the azimuth direction with a two element direction finding antenna (1, 2) having a fan pattern and wherein the path differences and Doppler frequencies are ranged selective to determine at each azimuth from the echo signals received a mean aspect angle (ε) and the azimuth maximum Doppler frequency which can be calculated therefrom. The mean aspect angles (ε) are determined according to the values of the measured Doppler frequencies with the equation ε=arc cos (f d /f dmaxα ). In this angle determination, smaller aspect angles are determined according to the measurement of the range selective determined path differences. Subsequently, an image point vertical deflection which is proportional to the aspect angle is utilized for perspective terrain display. The invention can be employed with pulsed radar devices on-board aircraft L for terrain display and for obtaining navigation data.

대표청구항 ▼

1. A device for on-board orientation in vehicles, such as aircraft which move relative to the ground, comprising a beam antenna which is sharply angularly focused in azimuth and less sharply focused in elevation and which scans the terrain in azimuth by swinging the radiating energy from said antenn

1. A device for on-board orientation in vehicles, such as aircraft which move relative to the ground, comprising a beam antenna which is sharply angularly focused in azimuth and less sharply focused in elevation and which scans the terrain in azimuth by swinging the radiating energy from said antenna, a receiver receiving from said antenna at each azimuth angle from the terrain at the angular range illuminated by the vertical antenna pattern a mixture of echo signals having different transit times which are respectively, proportional to the range of the respectively reflecting terrain elements and have different Doppler frequencies f d according to the relationship f s =f dmaxα ·cos=(2v Hα /λ)·cos ε, wherein v Hα is the aircraft velocity in the direction of the azimuth angle, λ is the radar wavelength and ε is the aspect angle of the appertaining terrain element, an image display device connected to said receiver for displaying a vertical image display of each azimuth angle which is illuminated by a plurality of radar wave trains, and the echo signals respectively received during successive time windows range gates and, thus, from successive distance range gate ranges and which are analyzed as to their Doppler frequencies, and said display device having a light spot for display on its picture screen which is vertically deflected proportional to the respective aspect angle, so that, in response to an echo received at a specific aspect angle and with a specific amplitude, the image spot is reproduced from such echo with a corresponding brightness and deflection which is proportional to the aspect angle, characterized in that the antenna is formed of at least two reception antenna rods (1 and 2) to form a direction-finding antenna and said antenna rods (1, 2) are mounted parallel to each other with a spacing of a few wavelengths, and the path difference (G) between echo signals received at the two reception antenna rods (1, 2) from the same terrain element (R) is determined by phase angle subtraction of the phase angles individually related to the range gate and is stored in a storing means, and the Doppler frequency is determined for each range gate, and the reference frequency ##EQU## is determined from the path differences and Doppler frequencies of at least two range gate ranges, wherein f di and f dj are the Doppler frequencies determined in the range gate ranges, G i and G j are the path differences determined in the appertaining range gate ranges, and s is the path difference steepness dependent on the respective aspect angle ε*, and for terrain representation on the radar screen, the light spot in at least one range (II) of mean aspect angles is vertically deflected approximately proportional to the magnitude ##EQU## wherein f d is the Doppler frequency which has been determined. 2. A device according to claim 1 characterized in that the direction-finding antenna has a separate transmission antenna rod mounted between two reception antenna rods (1, 2).