← Back to Patent Explorer
US4084158A Expired / Lapsed US ⏱️ 0.0 years remaining

Method of operating synthetic aperture radar

Assignee: Raytheon Co
•
Filing: 1977-01-03
•
Granted: 1978-04-11
•
Expires: 1997-01-03
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract A method, and apparatus for performing the method, of compensating for the effects of Doppler accelerations due to the orientation of the beam in a squinted synthetic aperture radar used for mapping terrain underlying an aircraft are described. According to the disclosed method, compensation is achieved by calculating the Doppler frequency shifts to be experienced by echo signals from points on the terrain to be mapped and then, in accordance with such calculations, varying the pulse repetition frequency of the squinted synthetic aperture radar to eliminate the effects of Doppler acceleration from the echo signals.

Inventors

  • 👤 Nathan Slawsby

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-23 22:18
CPC Classifications
G; G01; G01S; G01S13/00; G01S13/02; G01S13/50; G01S13/58; G01S13/60; G01S13/88; G01S13/89; G01S13/90; G01S13/904; G01S13/9041

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 113 words
An airborne coherent pulse Doppler radar including a Fast Fourier Transform signal processor adapted for use in an aircraft for the generation of real-time high resolution ground map imagery using synthetic aperture techniques, such radar comprising: (a) means for monitoring the attitude of said aircraft; (b) a motion compensation computer responsive to the velocity of the aircraft and the pulse repetition frequency of the radar for the generation of phase multipliers used by said processor to maintain the data from said radar in range focus; and, (c) means, responsive to said motion compensation computer, for varying the pulse repetition frequency of the radar to maintain the data from said radar in azimuth focus.
Claim 2
Dependent Claim 113 words
An airborne coherent pulse Doppler radar including a Fast Fourier Transform signal processor adapted for use in an aircraft for the generation of real-time high resolution ground map imagery using synthetic aperture techniques, such radar comprising: (a) means for monitoring the attitude of said aircraft; (b) a motion compensation computer responsive to the velocity of the aircraft and the pulse repetition frequency of the radar for the generation of phase multipliers used by said processor to maintain the data from said radar in range focus; and, (c) means, responsive to said motion compensation computer, for varying the pulse repetition frequency of the radar to maintain the data from said radar in azimuth focus.
Claim 3
Dependent Claim 87 words
In an airborne coherent side-looking radar having a Fast Fourier Transform signal processor for the generation of real-time high resolution ground map imagery by means of synthetic aperture techniques, and including compensatory phase shift means responsive to the aircraft velocity and the pulse repetition frequency of the radar for maintaining the data from the radar receiver in range focus, the improvement comprising means for varying, in a predetermined manner, the pulse repetition frequency of the radar to maintain the data from the radar receiver in azimuth focus.
Claim 4
Dependent Claim 87 words
In an airborne coherent side-looking radar having a Fast Fourier Transform signal processor for the generation of real-time high resolution ground map imagery by means of synthetic aperture techniques, and including compensatory phase shift means responsive to the aircraft velocity and the pulse repetition frequency of the radar for maintaining the data from the radar receiver in range focus, the improvement comprising means for varying, in a predetermined manner, the pulse repetition frequency of the radar to maintain the data from the radar receiver in azimuth focus.

References Cited (Backward Citations)

US3341847A Cited
US3737900A Cited
US3768096A Cited
US4034370A Cited
US3787848A Cited
US3987285A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1981-04-10 1981-10-10 1982-04-11 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1985-04-10 1985-10-10 1986-04-11 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1989-04-10 1989-10-10 1990-04-11 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag