HIGH INTEGRITY RADIO ALTIMETER

• US 20090289834A1
• Filed: 05/23/2008
• Published: 11/26/2009
• Est. Priority Date: 05/23/2008
• Status: Abandoned Application

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Devensky, Walt
• Application Number:
  US12/126,658
• Publication Number:
  US 20090289834A1
• Time in Patent Office: Days
• US Class Current: 342/122
• CPC Class Codes: G01S 13/325 using transmission of coded signals, e.g. P.S.K. signals
• CPC Class Codes: G01S 13/34 using transmission of continuous, frequency-modulated waves while heterodyning the received signal, or a signal derived therefrom, with a locally-generated signal related to the contemporaneously transmitted signal
• CPC Class Codes: G01S 13/343 using sawtooth modulation
• CPC Class Codes: G01S 13/87 Combinations of radar systems, e.g. primary radar and secondary radar
• CPC Class Codes: G01S 13/882 for altimeters measuring height using barometric means G01C5/06
• CPC Class Codes: G01S 7/0234 Avoidance by code multiplex

Abstract

A radio altimeter having a high level of integrity is presented. The radio altimeter includes a processing path configured to process a return signal received from a receive antenna using a first modulation technique and a monitoring path configured to process the return signal received from the receive antenna using a second modulation technique.

Claims

1. A radio altimeter having a high level of integrity, comprising:

a processing path configured to process a return signal received from a receive antenna using a first modulation technique; and

a monitoring path configured to process the return signal received from the receive antenna using a second modulation technique.

2. The radio altimeter of claim 1, wherein the processing path includes a first portion and a second portion,

the first portion configured to transmit a signal implementing the first modulation technique and the second modulation technique from a transmit antenna;

and

the second portion configured to process the return signal received from the receive antenna using the first modulation technique.

3. The radio altimeter of claim 2, wherein the first modulation technique comprises a frequency modulated continuous wave modulation technique.

4. The radio altimeter of claim 3, wherein the second modulation comprises code division multiple access modulation technique.

5. The radio altimeter of claim 2, wherein the processing path comprises a coupler, and wherein the first portion of the processing path comprises:

an exculsive OR gate;

a direct digital synthesizer configured to output frequency modulated continuous wave signals to the exculsive OR gate;

a phase-locked loop circuit configured to receive input signals from the exculsive OR gate and to output signals to the coupler; and

a code division multiple access code input configured to send signals to the exculsive OR gate and the phase-locked loop circuit, and wherein the coupler is configured to output signals to a transmit antenna and the second portion of the processing path;

wherein the second portion of the processing path comprises;

a mixer configured to receive the signals output from the coupler and from the receive antenna;

an amplifier configured to amplify an output of the mixer;

an analog-to-digital convertor configured to convert the amplified signal; and

a main processor to determine an altitude based on a delay in a code division multiple access code.

6. The radio altimeter of claim 1, further comprising:

a summing circuit configured to receive input from a first phase-locked loop circuit in the monitoring path and configured to receive input from a second phase-locked loop circuit in the processing path, the summing circuit operable to send an output to a transmit antenna wherein the code division multiple access modulation technique and the frequency modulated continuous wave modulation technique are implemented on signals sent from the transmit antenna.

7. The radio altimeter of claim 6, wherein the monitoring path comprises:

a direct digital synthesizer configured to output frequency modulated continuous wave signals to a first exculsive OR gate;

the first exculsive OR gate and a second exculsive OR gate configured to receive input from a code division multiple access code input;

a phase-locked loop circuit configured to receive output from the first exculsive OR gate; and

a coupler configured to receive output from the phase-locked loop circuit and configured to send output to the second exculsive OR gate.

8. The radio altimeter of claim 7, wherein the direct digital synthesizer is a first direct digital synthesizer, wherein the phase-locked loop circuit is a first phase-locked loop circuit, and wherein processing path comprises a first portion including:

a second direct digital synthesizer; and

a second phase-locked loop circuit communicatively coupled to receive input from the second direct digital synthesizer.

9. The radio altimeter of claim 8, wherein processing path further comprises a second portion including:

a mixer configured to receive the signals output from the second phase-locked loop circuit and from the receive antenna;

an amplifier configured to amplify an output of the first local oscillator;

an analog-to-digital convertor configured to convert the amplified signal; and

a main processor to determine an altitude based on a delay in a code division multiple access code.

10. The radio altimeter of claim 9, wherein the local oscillator is a first local oscillator, wherein

the first mixer mixes the output received from the second phase-locked loop circuit with the return signal received from the receive antenna and outputs information indicative of a frequency delay that is related to an altitude, and

wherein a second mixer mixes the output received from the second exculsive OR gate with the return signal received from the receive antenna and outputs information indicative of a code division multiple access-code delay that is associated with the altitude.

11. A method of providing a high level of integrity to an altitude determination, the method comprising:

modulating a signal sent over a first portion of a processing path in a radio altimeter according to a first modulation technique and a second modulation technique;

transmitting the modulated signal from a transmit antenna;

modulating a local oscillator signal sent to the processing path in the radio altimeter to extract the first modulation signal;

modulating a local oscillator signal sent to the monitoring path in the radio altimeter to extract the second modulation signal.

12. The method of claim 11, further comprising generating an altitude with a level of integrity greater than is obtained by processing the same signal through the processing and monitoring paths.

13. The method of claim 12, wherein the first modulation technique comprises a frequency modulated continuous wave modulation technique and the second modulation technique comprises a code division multiple access modulation technique,

wherein processing the return signal using the first modulation technique in the second portion of the processing path comprises sending the return signal over the second portion of the processing path to generate data indicative of a frequency delay;

and

wherein processing the return signal using the second modulation technique in the monitoring path comprises sending the return signal over the monitoring path to generate data indicative of a delay in a code division multiple access code.

14. The method of claim 13, further comprising:

receiving a return signal at a receive antenna;

splitting the return signal into two duplicate signals;

sending a first of the duplicate signals on the second portion of the processing path; and

sending a second of the duplicate signals on the monitoring path.

15. A radio altimeter system comprising

a first radio altimeter positioned in an aircraft;

and

a second radio altimeter positioned in the aircraft, each radio altimeter including;

a processing path configured to process a return signal received from a receive antenna using a first modulation technique to generate a first altitude; and

a monitoring path configured to process the return signal using a second modulation technique to generate a second altitude.

16. The radio altimeter system of claim 15, wherein the processing path in each radio altimeter includes a first portion and a second portion,

the first portion configured to transmit a signal implementing the first modulation technique and the second modulation technique from a transmit antenna, and

the second portion configured to process the return signal received from the receive antenna using the first modulation technique.

17. The radio altimeter system of claim 16, further comprising:

a first transmit antenna communicatively coupled to the first radio altimeter;

a first receive antenna communicatively coupled to the first radio altimeter;

a second transmit antenna communicatively coupled to the second radio altimeter; and

a second receive antenna communicatively coupled to the second radio altimeter.