Method and system for operating a vehicular electronic system with categorized voice commands

• US 8,224,653 B2
• Filed: 12/19/2008
• Issued: 07/17/2012
• Est. Priority Date: 12/19/2008
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: De Mers, Robert E., Nutaro, Joseph J., Grothe, Steven Paul
• Primary Examiner(s): Opsasnick, Michael N
• Application Number:
  US12/340,065
• Publication Number:
  US 20100161339A1
• Time in Patent Office: 1,306 Days
• Field of Search: 704/275
• US Class Current: 704/275
• CPC Class Codes: G10L 13/00 Speech synthesis; Text to speech systems
• CPC Class Codes: G10L 15/01 Assessment or evaluation of speech recognition systems
• CPC Class Codes: G10L 15/22 Procedures used during a speech recognition process, e.g. man-machine dialogue
• CPC Class Codes: G10L 2015/223 Execution procedure of a spoken command

Abstract

Methods and systems for operating an avionics system with voice command capability are provided. A first voice command is received. A first type of avionics system function is performed in response to the receiving of the first voice command. A second voice command is received. A second type of avionics system function that has a hazard level higher than that of the first type of avionics system function is performed in response to the receiving of the second voice command only after a condition is detected that is indicative of a confirmation of the request to perform the second type of avionics function. The avionics system may also have the capability to test whether or not the voice command feature is functioning properly.

Claims

1. A method for operating an avionics system comprising:

receiving a first voice command indicative of a request to perform a first type of avionics system function;

performing the first type of avionics system function in response to the receiving of the first voice command;

receiving a second voice command indicative of a request to perform a second type of avionics system function, the second type of avionics system function having a hazard level that is higher than that of the first type of avionics system function; and

performing the second type of avionics system function in response to the receiving of the second voice command only after a condition is detected that is indicative of a confirmation of the request to perform the second type of avionics function,

wherein the second voice command comprises at least one second voice command word and the confirmation voice command comprises the at least one second voice command word and a confirmation voice command word.

2. The method of claim 1, wherein the condition indicative of the confirmation of the request to perform the second type of avionics function comprises receiving a confirmation voice command indicative of the confirmation of the request to perform the second type of avionics function.

3. The method of claim 2, wherein the second voice command is spoken by a first user and the confirmation voice command is spoken by a second user.

4. The method of claim 3, wherein the performing of the second type of avionics system function occurs only if the confirmation voice command is received within a predetermined amount of time after the receiving of the second voice command.

5. The method of claim 2, wherein second voice command and the confirmation voice command are spoken by a single user and further comprising prompting the single user for the confirmation voice command after the receiving of the second voice command.

6. The method of claim 1, wherein the condition indicative of the confirmation of the request to perform the second type of avionics function comprises an operational state of an aircraft in which the avionics system is installed.

7. An avionics system comprising:

at least one microphone configured to detect voice commands and generate voice command signals representative thereof; and

a processing system in operable communication with the microphone, the processing system being configured to;

receive a first voice command signal from the at least one microphone, the first voice command signal being indicative of a request to perform a first type of avionics system function;

perform the first type of avionics system function in response to said receiving the first voice command signal;

receive a second voice command signal from the at least one microphone, the second voice command signal being indicative of a request to perform a second type of avionics system function, the second type of avionics system function having a hazard level that is higher than that of the first type of avionics system function; and

perform the second type of avionics system function in response to said receiving the second voice command only after a condition is detected that is indicative of a confirmation of the request to perform the second type of avionics function,

wherein the second voice command comprises at least one second voice command word and the confirmation voice command comprises the at least one second voice command word and a confirmation voice command word.

8. The avionics system of claim 7, wherein the condition indicative of the confirmation of the request to perform the second type of avionics function comprises receiving a confirmation voice command signal from the at least one microphone, the confirmation voice command signal being indicative of the confirmation of the request to perform the second type of avionics function.

9. The avionics system of claim 8, wherein the first, second, and confirmation voice command signals are generated by the at least one microphone upon receiving respective first, second, and confirmation voice commands.

10. The avionics system of claim 9, wherein the at least one microphone comprises first and second microphones, and the second voice command is received by the first microphone and the confirmation voice command is received by the second microphone.

11. The avionics system of claim 10, wherein the processing system is further configured such that the performing of the second type of avionics system function occurs only if the confirmation voice command signal is received within a predetermined amount of time after the receiving of the second voice command signal.

12. The avionics system of claim 9, wherein the second voice command and the confirmation voice command are received by a single microphone and wherein the processing system is further configured to generate a prompt for the confirmation voice command after the receiving of the second voice command signal.

13. The avionics system of claim 7, further comprising a speaker in operable communication with the processing system and being configured to generate an artificial voice command that is detectable by the at least one microphone and wherein the processing system is further configured to:

provide the speaker with a test voice command signal such that the speaker generates the artificial voice command;

receive an artificial voice command signal from the at least one microphone; and

compare the test voice command signal with the artificial voice command signal.

14. An avionics system comprising:

a speaker configured to generate an artificial voice command;

a microphone configured to detect the artificial voice command and generate an artificial voice command signal representative thereof; and

a processing system in operable communication with the speaker and the microphone, the processing system being configured to;

provide the speaker with a test voice command signal such that the speaker generates the artificial voice command;

receive the artificial voice command signal from the microphone; and

compare the test voice command signal with the artificial voice command signal.

15. The avionics system of claim 14, wherein the processing system is further configured to:

receive a first voice command signal from the microphone, the first voice command signal being generated by the microphone in response to receiving a first voice command indicative of a request to perform a first type of avionics system function; and

perform the first type of avionics system function in response to said receiving the first voice command signal based on the comparing the test voice command signal with the artificial command signal.

16. The avionics system of claim 15, further comprising a headset configured to be worn by a user and wherein the speaker and the microphone are coupled to the headset.

17. The avionics system of claim 16, wherein the processing system is further configured to:

receive a second voice command signal from the microphone, the second voice command signal being indicative of a request to perform a second type of avionics system function, the second type of avionics system function having a hazard level that is higher than that of the first type of avionics system function; and

perform the second type of avionics system function in response to the receiving the second voice command based on the comparing the test voice command signal with the artificial command signal only after a condition is detected that is indicative of a confirmation of the request to perform the second type of avionics function.

18. The avionics system of claim 17, wherein the condition indicative of the confirmation of the request to perform the second type of avionics function comprises receiving a confirmation voice command indicative of the confirmation of the request to perform the second type of avionics function and wherein the second voice command comprises at least one second voice command word and the confirmation voice command comprises the at least one second voice command word and a confirmation voice command word.