Radio altimeter for detecting accurate height

Patent metadata

Field	Value
Publication number	US-9720077-B1
Application number	US-201414255399-A
Country	US
Kind code	B1
Filing date	Apr 17, 2014
Priority date	Apr 17, 2014
Publication date	Aug 1, 2017
Grant date	Aug 1, 2017

Abstract

A method and system for adjusting a gain from a receiver antenna. The method may include accessing a radio altimeter data structure for antenna gain data. The antenna gain data may be associated with one or more antennas including a receiver antenna. Additionally, the method may include receiving aircraft maneuver data from a reference system. Furthermore, the method may include adjusting a gain from the receiver antenna based at least on the aircraft maneuver data.

First claim

What is claimed is:

1. A method, comprising:
accessing a radio altimeter data structure for predetermined antenna gain data, the predetermined antenna gain data being associated with one or more antennas including a receiver antenna implemented in a radio altimeter system of an aircraft, the predetermined antenna gain data including data of expected gains for reflected signals relative to possible angles for the reflected signals, the predetermined antenna gain further including an expected gain for a reflected signal at an antenna bore site angle, expected gains at angles corresponding to a main lobe of a radiation pattern of the receiver antenna, and expected gains at angles corresponding to side lobes of the radiation pattern of the receiver antenna;
receiving aircraft maneuver data from a reference system;
adjusting a gain from the receiver antenna based at least on the aircraft maneuver data and the predetermined antenna gain data, wherein adjusting the gain from the receiver antenna based at least on the aircraft maneuver data and the predetermined antenna gain data further comprises:
increasing an intermediate frequency gain from the receiver antenna to equal the expected gain for the reflected signal at the antenna bore site angle based at least on the aircraft maneuver data and the predetermined antenna gain data; and

determining a radio altimeter height based at least on the adjusted gain.

2. The method of claim 1 , wherein the aircraft maneuver data includes at least one of aircraft pitch data and aircraft roll data.

3. The method of claim 1 , wherein the reference system includes at least one of an inertial reference system and an attitude and heading reference system.

4. A method, comprising:
receiving weather radar data;
determining whether precipitation attenuation of signal transmission of a transmitter antenna implemented in a radio altimeter system of an aircraft is occurring based at least on the weather radar data;
determining a magnitude of the precipitation attenuation based at least on the weather radar data upon a determination that the precipitation attenuation of the signal transmission of the transmitter antenna is occurring;
amplifying a signal power of the transmitter antenna based at least on the magnitude of the precipitation attenuation upon determining the magnitude of the precipitation attenuation;
accessing a radio altimeter data structure for predetermined antenna gain data, the predetermined antenna gain data being associated with one or more antennas including a receiver antenna implemented in the radio altimeter system of the aircraft, the predetermined antenna gain data including data of expected gains for reflected signals relative to possible angles for the reflected signals, the predetermined antenna gain further including an expected gain for a reflected signal at an antenna bore site angle, expected gains at angles corresponding to a main lobe of a radiation pattern of the receiver antenna, and expected gains at angles corresponding to side lobes of the radiation pattern of the receiver antenna;
receiving aircraft maneuver data from a reference system;
adjusting a gain from the receiver antenna based at least on the aircraft maneuver data and the predetermined antenna gain data, wherein adjusting the gain from the receiver antenna based at least on the aircraft maneuver data and the predetermined antenna gain data further comprises:
increasing an intermediate frequency gain from the receiver antenna to equal the expected gain for the reflected signal at the antenna bore site angle based at least on the aircraft maneuver data and the predetermined antenna gain data; and

determining a radio altimeter height based at least on the adjusted gain.

5. A radio altimeter system, comprising:
a receiver antenna implemented in a radio altimeter system of an aircraft;
at least one computer readable medium; and
one or more processors, each of the one or more processors being coupled to one or more of the at least one computer readable medium, wherein the one or more processors are configured to execute instructions for:
accessing a radio altimeter data structure for predetermined antenna gain data, the predetermined antenna gain data being associated with one or more antennas including the receiver antenna, the predetermined antenna gain data including data of expected gains for reflected signals relative to possible angles for the reflected signals, the predetermined antenna gain further including an expected gain for a reflected signal at an antenna bore site angle, expected gains at angles corresponding to a main lobe of a radiation pattern of the receiver antenna, and expected gains at angles corresponding to side lobes of the radiation pattern of the receiver antenna;
receiving aircraft maneuver data from a reference system;
adjusting a gain from the receiver antenna based at least on the aircraft maneuver data and the predetermined antenna gain data, wherein adjusting the gain from the receiver antenna based at least on the aircraft maneuver data and the predetermined antenna gain data further comprises:
increasing an intermediate frequency gain from the receiver antenna to equal the expected gain for the reflected signal at the antenna bore site angle based at least on the aircraft maneuver data and the predetermined antenna gain data; and

determining a radio altimeter height based at least on the adjusted gain.

6. The radio altimeter system of claim 5 , further comprising:
a transmitter antenna implemented in the radio altimeter system.

7. The radio altimeter system of claim 6 , wherein the one or more processors are further configured to execute instructions for:
amplifying a signal power of the transmitter antenna.

8. The radio altimeter system of claim 6 , wherein the one or more processors are further configured to execute instructions for:
determining whether precipitation attenuation of signal transmission is occurring; and
amplifying a signal power of the transmitter antenna upon a determination that the precipitation attenuation of signal transmission is occurring.

9. The radio altimeter system of claim 6 , wherein the one or more processors are further configured to execute instructions for:
receiving weather radar data;
determining whether precipitation attenuation of signal transmission is occurring based at least on the weather radar data; and
amplifying a signal power of the transmitter antenna based at least on the weather data upon a determination that the precipitation attenuation of signal transmission is occurring.

10. The radio altimeter system of claim 6 , wherein the one or more processors are further configured to execute instructions for:
receiving weather radar data;
determining whether precipitation attenuation of signal transmission is occurring based at least on the weather radar data;
determining a magnitude of the precipitation attenuation based at least on the weather radar data; and
amplifying a signal power of the transmitter antenna based at least on the magnitude of the precipitation attenuation upon a determination that the precipitation attenuation of signal transmission is occurring.

Assignees

• Rockwell Collins Inc

Inventors

• Sarpoolaki Madjid N

Classifications

• G01S13/882

  for altimeters (measuring height using barometric means G01C5/06) · CPC title

• G01S13/953

  mounted on aircraft · CPC title

• G01S13/003

  Bistatic radar systems; Multistatic radar systems · CPC title

• G01S7/34

  Gain of receiver varied automatically during pulse-recurrence period, e.g. anti-clutter gain control · CPC title

• G01S13/02 Primary

  Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems · CPC title