System and method to automatically configure an aircraft for an operational flight phase

• US 8,493,240 B1
• Filed: 06/23/2010
• Issued: 07/23/2013
• Est. Priority Date: 07/16/2009
• Status: Active Grant

• Current Assignee: Rockwell Collins, Inc. (Rtx Corporation)
• Original Assignee: Rockwell Collins, Inc. (Rtx Corporation)
• Inventors: Carrico, Matthew J.
• Primary Examiner(s): PHAM, TOAN NGOC
• Application Number:
  US12/821,335
• Time in Patent Office: 1,126 Days
• Field of Search: 340/971, 340/945, 340/951, 340/963, 340/964, 715/859, 715/860, 715/771, 715/772, 701/9, 701/14, 701/15, 701/16
• US Class Current: 340/971
• CPC Class Codes: G01R 31/008 on air- or spacecraft, railway rolling stock or sea-going vessels
• CPC Class Codes: G05D 1/101 specially adapted for aircraft
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/0047 Navigation or guidance aids for a single aircraft details of equipment G08G5/0017

Abstract

An operational flight phase determination, indication and configuration system for an aircraft includes input/output circuitry for receiving an operational flight phase selector output signal, aircraft sensor signals, and on-board automation system output signals including configuration status information. A processor is coupled to the input/output circuitry. A flight phase data table is coupled to the processor. The flight phase data table includes a list of the defined operational flight phases for the aircraft. A flight phase transition rules set is coupled to the processor. The flight phase transition rules set includes flight rules for defining flight phase transitions. An aircraft system configuration data table is coupled to the processor. The aircraft system configuration data table includes a list of the defined configurations for each operational flight phase and the aircraft system configuration settings for each configuration. Program memory and working memory are coupled to the processor. The processor uses input from the input/output circuitry, the flight phase data table, the flight phase transition rules set, the program memory, the working memory, and the aircraft system configuration data table to provide an operational mode signal indicating the operational mode of the aircraft and a configuration command signal. A display indicator driver is coupled to the processor for providing display indicator driver signals to an operational flight phase indicator in accordance with the operational mode signal. Output drivers are coupled to the processor for providing configuration commands to aircraft systems in accordance with the configuration command signal.

Claims

1. An operational flight phase determination, indication and configuration system for an aircraft, comprising:

a) input/output circuitry for receiving an operational flight phase selector output signal, aircraft sensor signals, and on-board automation system output signals including configuration status information;

b) a processor coupled to said input/output circuitry;

c) a flight phase data table coupled to said processor, said flight phase data table including a list of the defined operational flight phases for the aircraft;

d) a flight phase transition rules set coupled to said processor, said flight phase transition rules set including flight rules for defining flight phase transitions;

e) an aircraft system configuration data table coupled to said processor, said aircraft system configuration data table including a list of the defined configurations for each operational flight phase and the aircraft system configuration settings for each said configuration;

f) program memory and working memory coupled to said processor, wherein said processor uses input from said input/output circuitry, said flight phase data table, said flight phase transition rules set, said program memory, said working memory and said aircraft system configuration data table to provide an operational mode signal indicating the operational mode of the aircraft and a configuration command signal;

g) a display indicator driver coupled to said processor for providing display indicator driver signals to an operational flight phase indicator in accordance with said operational mode signal; and

,

h) a plurality of output drivers coupled to said processor for providing configuration commands to aircraft systems in accordance with said configuration command signal.

2. The operational flight phase determination, indication and configuration system of claim 1 further comprising an airport map database coupled to said processor, airport map database information being used to infer the operational phase that the aircraft is in when the airplane is on the ground.

3. The operational flight phase determination, indication and configuration system of claim 1 wherein said operational mode signal provides an operational mode selected from the group of aircraft modes consisting of:

Pre-flight, Push back, Engine start, Ramp taxi out, Taxi out, De-ice, Take off, Climb, Cruise, Descent, Approach, Missed Approach, Landing, Rollout, Taxi off, Taxi in, Ramp taxi in, Engine shutdown, Post flight, Emergency, and Return to service engine check.

4. The operational flight phase determination, indication and configuration system of claim 1 wherein said operational mode signal provides an operational mode defined by the manufacturer or operator.

5. The operational flight phase determination, indication and configuration system of claim 1 wherein said processor operates to implement the steps comprising:

a) reading said flight phase data table;

b) reading in said aircraft system configuration data table;

c) reading said flight phase transition rules table;

d) reading said aircraft sensor signals;

e) reading said operational flight phase selector output signal;

f) reading said on-board automation system output signals;

g) determining from said read flight phase data table, said read aircraft system configuration data table, said read flight phase transition rules table, said aircraft sensor signals, and said operational flight phase selector output signal whether the aircraft is on the ground;

h) computing said flight phase from said read flight phase data table, said read flight phase transition rules table, said aircraft sensor signals, and said operational flight phase selector output signal, thus providing said operational mode signal;

i) computing said aircraft configuration from said read aircraft system configuration data table, said read on-board automation system output signals, and said operational mode signal, thus providing a configuration command signal;

j) providing said operational mode signal to a flight phase indicator;

k) providing said configuration command signal to an aircraft system; and

,

l) repeating steps d) through j).

6. The operational flight phase determination, indication and configuration system of claim 5 further including a step, between step k) and l), above, of using said aircraft sensor signals and said on-board automation system output signals to confirm the aircraft system is properly configured in accordance with said configuration command signal.

7. The operational flight phase determination, indication and configuration system of claim 1 wherein said processor operates to implement the step of computing said flight phase, by the steps of:

a) obtaining said list of defined operational flight phases from said flight phase data table;

b) obtaining said flight rules from said flight phase transition rules set;

c) determining whether a flight phase transition is occurring by obtaining said aircraft sensor signals, said operational flight phase selector output signal, and on-board automation system output signals as inputs from said input/output circuitry;

d) determining the initial operational state by applying said flight rules based on said inputs; and

,

e) monitoring said inputs and transitioning to the next operational state when said transition rules are satisfied by said inputs.

8. The operational flight phase determination, indication and configuration system of claim 1 further comprising an operational flight phase selector selecting a desired flight phase and providing said operational flight phase selector output signal in response to said selection.

9. The operational flight phase determination, indication and configuration system of claim 1 further comprising an operational flight phase indicator for receiving said display indicator driver signals and providing an indication of the active operational flight phase.

10. The operational flight phase determination, indication and configuration system of claim 1 wherein said configuration commands are implemented according to the interface requirements of the airplane systems being commanded.

11. The operational flight phase determination, indication and configuration system of claim 1 wherein when an aircraft system is not capable of responding to said configuration command signal, said configuration command is displayed on said operational flight phase indicator for manual setting thereof.

12. A method for determining, indicating, and configuring an operational flight phase of an aircraft, comprising:

a) receiving an operational flight phase selector output signal, aircraft sensor signals, and on-board automation system output signals including configuration status information, utilizing input/output circuitry;

b) providing an operational mode signal indicating the operational mode of the aircraft and a configuration command signal, utilizing a processor, using input from said input/output circuitry, a flight phase data table, a flight phase transition rules set, an aircraft system configuration data table, program memory and working memory, wherein, said flight phase data table includes a list of the defined operational flight phases for the aircraft, said flight phase transition rules set include flight rules for defining flight phase transitions, said aircraft system configuration data table includes a list of the defined configurations for each operational flight phase and the aircraft system configuration settings for each said configuration;

c) providing display indicator driver signals in accordance with said operational mode signal;

d) providing a plurality of output drivers coupled to said processor for providing configuration commands to aircraft systems in accordance with said configuration command signal;

e) displaying the active operational flight phase of the aircraft in response to said display indicator driver signals; and

,

f) configuring aircraft systems in response to said configuration command signal.

13. The method of claim 12 wherein said processor operates to implement the steps, comprising:

a) reading said flight phase data table;

b) reading in said aircraft system configuration data table;

c) reading said flight phase transition rules table;

d) reading said aircraft sensor signals;

e) reading said operational flight phase selector output signal;

f) reading said on-board automation system output signals;

g) determining from said read flight phase data table, said read aircraft system configuration data table, said read flight phase transition rules table, said aircraft sensor signals, and said operational flight phase selector output signal whether the aircraft is on the ground;

h) computing said flight phase from said read flight phase data table, said read flight phase transition rules table, said aircraft sensor signals, and said operational flight phase selector output signal, thus providing said operational mode signal;

i) computing said aircraft configuration from said read aircraft system configuration data table, said read on-board automation system output signals, and said operational mode signal, thus providing a configuration command signal;

j) providing said operational mode signal to a flight phase indicator;

k) providing said configuration command signal to an aircraft system; and

,

l) repeating steps d) through j).

14. An aircraft configuration determination system, comprising:

a) input/output circuitry for receiving a configuration selector output signal; and

, on-board automation system output signals including configuration status information;

b) a processor coupled to said input/output circuitry;

c) an aircraft system configuration data table coupled to said processor, said aircraft system configuration data table including a list of the defined configurations for each configuration selectable by a configuration selector;

d) program memory and working memory coupled to said processor, wherein said processor uses input from said input/output circuitry, said program memory, said working memory and said aircraft system configuration data table to provide a configuration mode signal indicating the selected configuration mode of the aircraft and a configuration command signal;

e) a display indicator driver coupled to said processor for providing display indicator driver signals to a configuration indicator in accordance with said configuration mode signal; and

,

f) a plurality of output drivers coupled to said processor for providing configuration commands to aircraft systems in accordance with said configuration command signal.

15. The operational flight aircraft configuration determination system of claim 14 wherein when an aircraft system is not capable of responding to said configuration command signal, said configuration command is displayed on said configuration indicator for manual setting thereof.