Decorrelation tolerant coherent radar altimeter

• US 4,851,852 A
• Filed: 04/20/1987
• Issued: 07/25/1989
• Est. Priority Date: 04/20/1987
• Status: Expired due to Fees

• Current Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Original Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Inventors: Thue, Baard H., Bjorke, Merlin D.
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): GREGORY, BERNARR E
• Application Number:
  US07/040,436
• Time in Patent Office: 827 Days
• Field of Search: 342/120-124, 342/128-132, 342/134, 342/135, 342/202-204
• US Class Current: 342/120
• CPC Class Codes: G01S 13/10 using transmission of interrupted, pulse modulated waves determination of distance by phase measurement G01S13/32
• CPC Class Codes: G01S 13/32 using transmission of continuous waves, whether amplitude-, frequency-, or phase-modulated, or unmodulated
• CPC Class Codes: G01S 13/882 for altimeters measuring height using barometric means G01C5/06
• CPC Class Codes: G01S 7/28 Details of pulse systems

Abstract

A pulsed coherent radar altimeter is described which employs a narrow band receiver and utilizes a novel digital coherent pulse generator. A coherent pulse radar transmits a pulse comprised of the sum of at least two phase related RF signals closely spaced in frequency. The phase shift due to platform motion and return surface irregularity of the return signal is approximately the same for each carrier. The receiver produces a signal representative of the difference of the two carriers which is substantially free of decorrelation effects, and which can be processed in a narrow band receiver to produce range information.

Claims

1. A coherent radar altimeter system comprising in combination:

signal generating means for generating a series of coherent radar pulse signals having a high frequency carrier in which said high frequency carrier is comprised of two co-existing high frequency signal components of a first and a second frequency, respectively, closely spaced in frequency;

means to transmit said series of coherent radar pulses;

means for receiving return signal pulses, said return signal pulses being said transmitted pulses reflected from a target surface;

means for processing said return signal pulses, including means for producing from said return signal pulses a signal which is representative of the difference between first and second return signal components of said returned signal pulses in which said first return signal component is of said first frequency and said second return signal component is of said second frequency.

2. A coherent radar altimeter system as in claim 1 wherein said means for processing said return signal includes a pair of filters respectively centered at said first and second frequencies, a mixer, means to couple the output of each of said filters to said mixer, a narrow band filter, and means to couple the output of said mixer to said narrow band filter.

3. A coherent radar altimeter system as in claim 2 wherein said narrow band filter has a prediction bandwidth equal to the information bandwidth.

4. A coherent radar altimeter system as in claim 3 wherein said narrow band filter has a center frequency substantially equal to the frequency difference between said first and second frequencies.

5. The coherent radar altimeter of claim 1 wherein said signal generating means includes:

a high frequency oscillator providing a first signal;

a controllable bi-phase modulating switch having input means for receiving said first signal, and a control input means for receiving a control signal, and an output means;

a pair of phase related pulse generators for providing first and second pulse trains; and

means for obtaining a product signal representative of the product of said first and second pulse trains, said product signal providing said control signal.

6. A coherent radar altimeter system comprising in combination:

a signal generator for generating an RF signal comprised of two phase related frequency components, said signal generator including,

a high frequency oscillator for generating a first RF signal,

a pair of phase related pulse generators for providing first and second pulse trains;

first means responsive to said first and second pulse train signals for providing a product signal representative of the product of said first and second pulse train signals, and

a controllable bi-phase modulating switch having input means connected to the output of said high frequency oscillator, and an output means, said switch including control means for receiving said product signal, said switch means operative to pass said first RF signal to said output means in response to a first condition of said first product signal, and passing said first RF signal to said output means with 180°

phase inversion in response to a second condition of said product signal;

means to transmit said series of coherent radar pulses;

means for receiving return signals from said transmitted pulses from a target surface; and

means for processing said return pulses, including means for producing from said return pulses a signal which is representative of the difference between first and second return signal components of said returned signal pulses in which said first return signal component is of said first frequency and said second return signal component is of said second frequency.