Operational flight phase determination and indication system

• US 8,217,807 B1
• Filed: 07/16/2009
• Issued: 07/10/2012
• Est. Priority Date: 07/16/2009
• Status: Active Grant

• Current Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Carrico, Matthew J.
• Primary Examiner(s): Pham, Toan N
• Application Number:
  US12/504,524
• Time in Patent Office: 1,090 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: 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 and indication system for an aircraft includes input/output circuitry for receiving an operational flight phase selector output signal and aircraft sensor signals. 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. 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 and the working memory to provide an operational mode signal indicating the operational mode of the aircraft. A flight phase selector is coupled to the processor for providing the flight phase selector signal to the processor in accordance with the pilot selected flight phase input. 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. The input/output circuitry preferably receives on-board automation systems input.

Claims

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

a) input/output circuitry for receiving an operational flight phase selector output signal and aircraft sensor signals;

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) 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 and said working memory to provide an operational mode signal indicating the operational mode of the aircraft; and

,

f) 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.

2. The operational flight phase determination and indication system of claim 1 wherein said input/output circuitry receives on-board automation system output signals for use in determining the flight phase and flight phase transitions, and said processor provides said operational mode signal to an on-board automation system.

3. The operational flight phase determination and indication 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.

4. The operational flight phase determination and indication system of claim 3 wherein said processor operates to implement the steps comprising:

a) reading said flight phase data table;

b) reading said flight phase transition rules table;

c) reading said aircraft sensor signals;

d) reading said operational flight phase selector output signal;

e) determining 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 whether the aircraft is on the ground;

f) 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;

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

,

h) repeating steps c) through f).

5. The operational flight phase determination and indication system of claim 4 wherein said processor further operates to implement a step of providing said operational mode signal to a communication system.

6. The operational flight phase determination and indication system of claim 4 wherein said processor further operates to reading on-board automation system output signals from on-board automation systems prior to determining whether the system is on the ground.

7. The operational flight phase determination and indication system of claim 4 wherein said processor further operates to implement a step of providing said operational mode signal to on-board automation systems.

8. The operational flight phase determination and indication system of claim 4 wherein said processor further operates to implement the steps of:

determining the airport and reading said airport map database information if the airplane is on the ground.

9. The operational flight phase determination and indication 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.

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

11. The operational flight phase determination and indication system of claim 1 wherein said input/output circuitry receives communication system output signals for use in determining the flight phase and flight phase transitions, and said processor provides said operational mode signal to a communication system.

12. The operational flight phase determination and indication 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 the said inputs.

13. The operational flight phase determination and indication 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.

14. The operational flight phase determination and indication 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.

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

a) an input device for selecting the desired flight phase and providing an operational flight phase selector output signal;

b) processing and generating means for processing said operational flight phase selector output signal and generating a display indicator driver signal, said processing and generating means including a flight phase data table including a list of the defined operational flight phases for the aircraft, and a flight phase transition rules set including flight rules for defining flight phase transitions; and

,

c) a display device for receiving said display indicator driver signal and indicating the active operational flight phase.

16. The operational flight phase determination and indication system of claim 15 wherein said flight phase selector is a mechanical mechanism comprising a rotary knob or a pushbutton.

17. The operational flight phase determination and indication system of claim 15 wherein said flight phase selector is a selectable item on a display.

18. The operational flight phase indicator of claim 15 wherein said flight phase indicator is a discrete lamp that illuminates to indicate the active mode.

19. The operational flight phase indicator of claim 15 wherein said flight phase indicator is shown on a display.

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

a) selecting an operational flight phase and generating an operational flight phase selector output signal in response to said selection;

b) utilizing input/output circuitry for receiving said operational flight phase selector output signal and aircraft sensor signals;

c) providing an operational mode signal indicating the operational mode of the aircraft, using input from said input/output circuitry, a flight phase data table, a flight phase transition rules set, 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;

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

,

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