Angle-of-arrival measurement via time doppler shift

Communications: directive radio wave systems and devices (e.g. – Radar ew

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

342387, G01S 1350

Patent

active

052413136

ABSTRACT:
To allow measurement of the angle-of-arrival (AOA) of the radar pulses from an uncooperative ground-based emitter, the method exploits the time doppler shift resulting from the velocity of a high performance aircraft and the high maneuver ability available to such aircraft to form initial angle calculations. These initial angle calculations along with inherent radar stability are then used for subsequent AOA measurements. The aircraft is flown at a constant velocity V.sub.B along successive legs with an angle .phi..sub.K between successive legs, and the velocity V.sub.B and the angles .phi..sub.K are found using a navigation system such as GPS or inertial navigation. The time difference T.sub.n '-T.sub.1 ' is measured between the arrival of the first and last of n pulses for each sample. A general approximation equation of T.sub.n '-T.sub.1 ' is normalized such that for any K samples the following equation applies,

REFERENCES:
patent: 3866229 (1975-02-01), Hammack
patent: 4008470 (1977-02-01), Lanning et al.
patent: 4172255 (1979-10-01), Barrick et al.
patent: 4393382 (1983-07-01), Jones
patent: 4549184 (1985-10-01), Boles et al.
patent: 4746924 (1988-05-01), Lightfoot
patent: 4825213 (1989-04-01), Smrek

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Angle-of-arrival measurement via time doppler shift does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Angle-of-arrival measurement via time doppler shift, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Angle-of-arrival measurement via time doppler shift will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-2300835

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.