Vertical required navigation performance containment with radio altitude

• US 8,494,693 B2
• Filed: 08/05/2009
• Issued: 07/23/2013
• Est. Priority Date: 08/05/2009
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Murphy, Timothy Allen
• Primary Examiner(s): Nguyen, Cuong H
• Application Number:
  US12/535,731
• Publication Number:
  US 20110035080A1
• Time in Patent Office: 1,448 Days
• Field of Search: 701 8- 9, 701 4- 5, 701 15- 17, 701/18, 340/963, 340/972, 340/971, 340/967, 340/970, 340/977, 340/979, 340/974, 340/947, 340/951, 342/5, 342/122, 342/120, 342/33, 707/E17.044, 731/78.T, 731/78.R
• US Class Current: 701/18
• CPC Class Codes: B64D 45/04 Landing aids; Safety measures to prevent collision with earth's surface
• CPC Class Codes: G01C 23/00 Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
• CPC Class Codes: G01S 13/882 for altimeters measuring height using barometric means G01C5/06
• CPC Class Codes: G01S 19/32 Multimode operation in a single same satellite system, e.g. GPS L1/L2
• CPC Class Codes: G01S 7/003 Transmission of data between radar, sonar or lidar systems and remote stations
• CPC Class Codes: G05D 1/0676 specially adapted for landing
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/025 Navigation or guidance aids radar or analogous systems specially adapted for landing purposes G01S13/913

Abstract

A monitor on-board an aircraft which uses radio altitude measurements as the basic observable altitude during runway approach. The basic concept utilizes the aircraft'"'"'s navigation system, which includes means to store and retrieve radio altitude thresholds as a function of the distance along the desired path from the runway thresholds. These threshold functions are determined in advance based on a radio altitude reference which is defined as the expected radio altimeter measurement that would be made if the airplane were exactly on the desired reference path. Vertical containment monitoring is achieved by comparing the radio altitude measurement to computed thresholds for both too high and too low. During the approach, an annunciation message can be generated if the radio altitude measurement is above or below the threshold limits. Using this monitor ensures that the total system error for the aircraft is contained within a bound called the Vertical Containment Level of the desired reference path in space with a probability that is specified.

Claims

1. A method for detecting deviation of true airplane vertical position of an aircraft from a desired reference path, comprising the following steps:

acquiring radio altitude and GPS measurements over the course of multiple approaches by aircraft approaching a runway threshold;

deriving high and low radio altitude thresholds for a reference approach flight path from said acquired radio altitude and GPS measurements, wherein said high and low radio altitude thresholds vary as a function of horizontal distance from the runway threshold;

storing said high and low radio altitude thresholds on the aircraft;

acquiring radio altitude measurements as a function of horizontal distance from the runway threshold as the aircraft on which said high and low radio altitude thresholds are stored approaches the runway threshold; and

comparing each radio altitude measurement to a respective corresponding pair of said high and low radio altitude thresholds as the aircraft on which said high and low radio altitude thresholds are stored approaches the runway threshold.

2. The method as recited in claim 1, further comprising the step of generating an indicator that indicates a radio altitude measurement was higher than a high radio altitude threshold or lower than a low radio altitude threshold as the aircraft on which said high and low radio altitude thresholds are stored approaches the runway threshold.

3. The method as recited in claim 1, wherein said deriving step comprises computing said high and low radio altitude thresholds as a function of reference radio altitudes representing expected radio altitude measurements were the aircraft to travel along said reference approach flight path.

4. The method as recited in claim 2, further comprising displaying said indicator on a cockpit display.

5. The method as recited in claim 1, wherein in said comparing step each radio altitude measurement is compared to a respective corresponding pair of said high and low radio altitude thresholds corresponding to the horizontal distance of the aircraft from the runway threshold when the radio altitude measurement is made.

6. The method as recited in claim 1, wherein said high and low radio altitude thresholds are set to ensure an acceptable probability of false alarms.

7. The method as recited in claim 1, wherein said high and low radio altitude thresholds are not derived from a terrain database.

8. The method as recited in claim 1, wherein the aircraft is flying a vertical navigation path based on vertical guidance from a source which is independent of radio altitude.

9. A method for detecting deviation of true airplane vertical position of an aircraft from a desired reference path, comprising the following steps performed by a processing system onboard the aircraft:

(a) storing high and low radio altitude thresholds on an aircraft, wherein said high and low radio altitude thresholds vary as a function of horizontal distance from the runway threshold;

(b) acquiring radio altitude measurements as a function of horizontal distance from the runway threshold as the aircraft on which said high and low radio altitude thresholds are stored approaches the runway threshold;

(c) determining whether any of said radio altitude measurements are less than the corresponding low radio altitude thresholds as the aircraft approaches the runway threshold;

(d) determining whether any of said radio altitude measurements are greater than the corresponding high radio altitude thresholds as the aircraft approaches the runway threshold; and

(e) performing one of the following steps (i) through (iii) depending on the results of step (d);

(i) generating a first alert signal as the aircraft approaches the runway threshold if a determination is made that any of said radio altitude measurements are less than the corresponding low radio altitude thresholds;

(ii) generating a second alert signal as the aircraft approaches the runway threshold if a determination is made that any of said radio altitude measurements are greater than the corresponding high radio altitude thresholds; and

(iii) not generating either of said first and second alert signals as the aircraft approaches the runway threshold if a determination is made that said radio altitude measurements are less than the corresponding high radio altitude thresholds and greater than the corresponding low radio altitude thresholds.

10. The method as recited in claim 9, wherein said high and low radio altitude thresholds are set to ensure an acceptable probability of false alarms.

11. The method as recited in claim 9, wherein said high and low radio altitude thresholds are not derived from a terrain database.

12. The method as recited in claim 9, wherein in said comparing step, each radio altitude measurement is compared to a respective corresponding pair of said high and low radio altitude thresholds corresponding to the horizontal distance of the aircraft from the runway threshold when the radio altitude measurement is made.

13. The method as recited in claim 9, wherein if either of said first and second alert signals is generated, further comprising displaying on a cockpit display a visual indicator corresponding to said generated first or second alert signal.

14. The method as recited in claim 9, wherein if either of said first and second alert signals is generated, further comprising generating an alert annunciation corresponding to said generated first or second alert signal using either a tone generator or a voice simulator.