Low-cost radio altimeter

• US 5,719,581 A
• Filed: 02/12/1996
• Issued: 02/17/1998
• Est. Priority Date: 02/12/1996
• Status: Expired due to Fees

• Current Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Original Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Inventors: Poe, John J.
• Primary Examiner(s): Sotomayor, John B.
• Application Number:
  US08/599,736
• Time in Patent Office: 736 Days
• Field of Search: 342/120, 342/122, 342/128
• US Class Current: 342/120
• CPC Class Codes: G01C 5/005 altimeters for aircraft G01C5/02, G01C5/06 take precedence
• CPC Class Codes: G01S 13/345 using triangular modulation
• CPC Class Codes: G01S 13/882 for altimeters measuring height using barometric means G01C5/06
• CPC Class Codes: G01S 13/935 for terrain-avoidance

Abstract

A relatively low-cost FMCW radio altimeter includes a voltage-controlled oscillator based upon a GaAs FET. The oscillator produces, for example, a 4.3 GHz microwave signal that is modulated with a triangular wave having a pin-selectable modulation frequency. The modulated signal is amplified by a buffer amplifier, as well as a power amplifier, and connected to an RF output terminal by way of a plurality of microstrips. Reflected signals are received at an RF input and are coupled to a mixer by way of a low-noise amplifier. The modulation signal is also applied to the mixer by way of a microstrip coupling device to produce an audio output signal whose frequency is proportional to the altitude above ground. The gains of all of the amplifiers are selected to eliminate the need for hand-tuning of the microstrips and to enable the use of a glass/epoxy circuit board. The output of the radio altimeter is an audio signal whose frequency is proportional to the height above ground, which enables direct digital conversion by way of a frequency-to-binary converter.

Claims

1. A radio altimeter comprising:

a predetermined oscillator for generating an oscillation signal at a predetermined frequency;

means for modulating said oscillation signal with a predetermined modulation signal defining a modulated signal;

means for radiating said modulated signal defining a radiated modulated signal;

first means for coupling said modulated signal to said radiating means, said first coupling means including one or more radiating circuit microstrips;

means for amplifying said modulation signal, said amplifying means having a predetermined gain selected to eliminate the need to tune said one or more radiating circuit microstrips;

means for receiving a reflection of said radiated modulated signal defining reflection signals;

means for mixing said modulated signals with said reflection signals to generate an audio signal whose frequency is proportional to the altitude of the aircraft above ground;

second means for coupling said reflection signals to said mixing means, said second coupling means including one or more receiving circuit microstrips; and

means for amplifying said reflection signals, said amplifying means including a plurality of low-noise amplifiers, at least one of said low-noise amplifiers having a predetermined gain selected to eliminate the need to tune said one or more receiving circuit microstrips.

2. A radio altimeter as recited in claim 1, wherein said predetermined oscillator is a voltage controlled oscillator.

3. A radio altimeter as recited in claim 2, wherein said voltage-controlled oscillator includes a GaAs field-effect transistor (FET).

4. A radio altimeter as recited in claim 1, wherein said predetermined modulation signal is a triangular wave having a predetermined modulation frequency.

5. A radio altimeter as recited in claim 4, further including means for enabling manual selection of said modulation frequency from a plurality of modulation frequencies.

6. A radio altimeter as recited in claim 1, wherein said modulation signal amplifying means includes a predetermined buffer amplifier.

7. A radio altimeter as recited in claim 6, wherein said modulation signal amplifying means includes a power amplifier coupled to said buffer amplifier by way of said coupling means.

8. A radio altimeter as recited in claim 6, further including means for adjusting the operating set point of said buffer amplifier.

9. A radio altimeter as recited in claim 7, further including means for adjusting the set point of said power amplifier.

10. A radio altimeter as recited in claim 1, further including means for amplifying said reflection signals.

11. A radio altimeter as recited in claim 10, wherein said reflection signal amplifying means includes a low-noise amplifier (LNA) coupled to said mixing means and coupling means for coupling said LNA to said mixing means, said coupling means including one or more microstrips.

12. A radio altimeter as recited in claim 1, further including means for providing a signal representative of the gain of said modulation signals.

13. A radio altimeter comprising:

an oscillator for generating an oscillation signal at a predetermined frequency;

a modulator for generating a modulation signal for modulating said oscillation signal, said modulation signal being a triangular wave at a predetermined modulation frequency, defining a modulated signal;

a buffer amplifier having a predetermined gain for amplifying said modulated signal, said buffer amplifier being electrically coupled to said oscillator, said coupling including one or more microstrips;

a power amplifier having a predetermined gain, electrically coupled to said power amplifier, said coupling including one or more microstrips;

an RF output terminal electrically coupled to said power amplifier, said coupling including one or more microstrips;

an RF input terminal for receiving reflected signals;

a mixer for mixing said modulated signals with said reflected signals to generate a signal whose frequency is proportional to the altitude of the aircraft above ground;

a local oscillator coupling device which includes one or more microstrips for coupling said modulated signal to said mixer; and

a plurality of low-noise amplifiers, each of said amplifiers having a predetermined gain, said amplifiers electrically coupled to said RF input terminal and to said mixer by microstrips, wherein the gain of at least one of said amplifiers is selected to eliminate the need to tune said microstrips.

14. A radio altimeter as recited in claim 13, further including means for adjusting the operating point of said buffer amplifier.

15. A radio altimeter as recited in claim 13, further including means for adjusting the operating point of said power amplifier.

16. A radio altimeter as recited in claim 13, further including means for adjusting the operating point of at least one of said low-noise amplifiers.

17. A radio altimeter as recited in claim 13, wherein said circuit for generating said modulation circuit includes a counter for generating a square wave having a predetermined modulation frequency and means for integrating said square wave to generate a triangular wave modulation signal.

18. A radio altimeter as recited in claim 17, further including means for disabling said modulation signal for predetermined frequencies.

19. A radio altimeter as recited in claim 13, further including means for detecting the output level of said modulated signal and comparing it with a reference signal to generate a status signal representative of the level of the output signal.

20. A radio altimeter as recited in claim 13, wherein said radio altimeter is formed on a glass/epoxy circuit board.

21. A frequency modulated continuous wave radio altimeter comprising:

(a) a transmit circuit for transmitting a first signal;

(b) a receive circuit for receiving a reflection of said first signal and for producing a second signal indicative of a height above ground; and

(c) at least one of said transmit circuit or said receive circuit including;

(i) at least one microstrip circuit; and

(ii) a plurality of amplifiers electrically coupled to said microstrip circuit, said amplifiers having a gain selected to eliminate the need to tune said microstrip circuit.

22. The altimeter of claim 21 wherein said altimeter is fabricated on a glass/epoxy printed circuit board.

23. The altimeter of claim 21 wherein said amplifiers further include GaAs field effect transistors as active elements.