Air bag operation device

• US 5,422,965 A
• Filed: 02/12/1993
• Issued: 06/06/1995
• Est. Priority Date: 02/18/1992
• Status: Expired due to Fees

• Current Assignee: Hitachi, Ltd.
• Original Assignee: Hitachi, Ltd.
• Inventors: Sato, Hiroshi, Suzuki, Masayoshi, Tashiro, Korefumi, Bekki, Keisuke, Suzuki, Seiko
• Primary Examiner(s): Teska, Kevin J.
• Assistant Examiner(s): NGUYEN, TAN QUANG
• Application Number:
  US08/017,389
• Time in Patent Office: 844 Days
• Field of Search: 364/424.05, 364/424.03, 364/431.12, 280/735, 280/731, 280/729, 280/734, 307/10.1, 307/10.3, 307/10.6, 180/271, 180/274, 340/438, 340/436
• US Class Current: 701/47
• CPC Class Codes: B60R 21/0132 responsive to vehicle motion parameters , e.g. to vehicle longitudinal or transversal deceleration or speed value
• CPC Class Codes: B60R 21/0173 Diagnostic or recording means therefor
• CPC Class Codes: G01D 3/08 with provision for safeguarding the apparatus, e.g. against abnormal operation, against breakdown
• CPC Class Codes: G01P 21/00 Testing or calibrating of apparatus or devices covered by the preceding groups

Abstract

An air bag operation device which employs only one CPU module to guarantee sufficient fail-safety in the operation of the air bag without increasing the scale of the hardware. A plurality of crash-discriminating programs of different versions and a plurality of self-diagnosing programs of different versions are executed by a single CPU module, a signal is fed to an air bag igniting device based upon a comparison of the discriminated results by the plurality of crash-discriminating programs, and a signal is fed to an abnormality alarm device based upon comparison of the discriminated results of the plurality of self-diagnosing programs.

Claims

1. Method of operating an air bag igniter control apparatus have a crash sensor for detecting a condition indicative that a crash has occurred, a data processor, which evaluates signals from said sensor, and an abnormality indicator apparatus, said method comprising the steps of:

said data process continuously performing a self diagnostic function for detecting a failure in the data processor and a memory thereof when no signal is received from said sensor;

said data processor transmitting an abnormality signal to an abnormality indicator apparatus when a failure is detected;

wherein said self diagnostic function comprises the steps of;

executing a first version of a self diagnostic program which includes processing steps for checking for proper operation of at least said data processor, said memory, and a data bus of said data processor, and generating an output signal indicative of said proper operation;

executing a second version of said self diagnostic program which includes processing steps for checking for proper operation of at least said data processor, said memory, and a data bus of said data processor, and generating an output signal indicative of said proper operation, said processing steps and said output signal of said second version being different from said processing steps and said output signal of said first version; and

comparing output signals of said first version with output signals of said second version.

2. Method according to claim 1,

wherein in said first version of said self diagnostic program, said data processor produces a first predetermined binary data word if no error is detected in said apparatus, and in said second version of said self diagnostic program, said data processor produces a second predetermined binary data word if n o error is detected in said apparatus;

and

wherein bits of said second predetermined data word are complementary to corresponding bits of said first predetermined data word.

3. Method according to claim 2 wherein said comparing step comprises to steps of:

entering said first predetermined data word into a register in data processor;

reading contents of said register;

entering said second predetermined data word into said register in place of said first predetermined data word.

reading contents of said register;

Whereby when no error is detected in said apparatus, said reading steps generate a signal having a first predetermined frequency.

4. Method according to claim 3 comprising the further step of generating an alarm when said signal has a frequency other than said predetermined frequency.

5. Method of operating an air bag igniter control apparatus have a crash sensor for detecting a condition indicative that a crash has occurred, a data processor, which evaluates signals from said sensor, and an abnormality indicator apparatus, said method comprising the steps of:

said data process continuously performing a self diagnostic function for detecting a failure in the data processor and a memory thereof when no signal is received from said sensor;

said data processor transmitting an abnormality signal to an abnormality indicator apparatus when a failure is detected;

interrupting operation of said self diagnostic function when a signal is received from said crash sensor, indicating that a crash may have occurred; and

said data processor performing a crash discrimination function to determine whether a crash has occurred;

wherein said crash discrimination function comprises the steps of

executing a first version of a crash discriminating program which includes processing steps for checking for proper operation of at least said data processor, said memory, and a data base of said data processor, and generating an output signal indicative of said proper operation;

executing a second version of said self crash discrimination program which includes processing steps for checking for proper operation of at least said data processor, said memory, and a data base of said data processor, and generating an output signal indicative of said proper operation, said processing steps and said output signal of said second version being different from said processing steps and said output signal of said first version; and

comparing output signals of said first version with output signals of said second version.

6. Method according to claim 5,

wherein said data processor determines that a crash has occurred when said signal from said crash sensor exceeds a predetermined threshold value;

wherein in said first version of said crash discriminating program, said data processor produces a third predetermined binary data word if a crash has occurred, and a fourth predetermined binary data word if no crash has occurred;

wherein in said second version of said crash discriminating program, said data processor produces a fifth predetermined binary data word if a crash as occurred and a sixth predetermined binary data word if no crash has occurred; and

wherein bits contained in a first portion of said third binary data word are complementary to corresponding bits contained in a first portion of said fifth binary data word, and bits contained in a second portion of said fourth binary data word are complementary to corresponding bits of a second portion of said sixth binary data word.

7. Method according to claim 6 wherein said comparing step comprises the steps of:

entering the binary data word produced by said first version of said crash discriminating program into a register of said data processor;

reading contents of said register;

entering the binary data word produced by said second version of said crash discrimination program into said register;

reading contents of said register;

whereby when a crash is detected sequential reading of said first portion of said binary data words entered into said register produces a signal having a second predetermined frequency when a crash is detected, and sequential reading of said second portion of said binary data words entered into said register produces a signal having said second predetermined frequency.

8. Method according to claim 7 comprising the further step of generating an ignition signal when said signal generated by said first portion of said binary data words entered into said register has said second predetermined frequency.

9. Method of operating a vehicle air bag control system having a sensor for detecting a condition indicative that a crash has occurred, a single data processor which evaluates signals from said sensor, and an abnormality indicator apparatus, said method comprising the steps of:

said data processor continuously alternatively executing at least first and second versions of a self diagnostic program, said first and second versions of said self diagnostic program each including processing steps for checking for proper operation of at least said data processor, said memory and a data bus of said data processor, and generating a diagnostic signal indicative thereof, said processing steps and said diagnostic signal of said first version being different from said processing steps and said diagnostic signal of said second version;

comparing portion of said diagnostic signals generated by said first and second versions to generate a first diagnostic output signal when said air bag control system is operating without error, and a second diagnostic output signal when an error is detected.

10. Method of operating a vehicle air bag control system having a single data processor, comprising the steps of:

said data processor executing a first crash detection program to generate a first digital signal;

said data processor executing a second crash detection program to generate a second digital signal, said first and second crash detection programs each including processing steps to check for proper operation of at least said data processor and to generate said first and second digital signals, said processing steps and said first digital signals of said first crash detection program being different from said processing steps and second digital signals of said second crash detection program;

a first portion of said first digital signal comprising data bits which are complementary to data bits of a first portion of said second digital signal when a crash has occurred, and a second portion of said first digital signal comprising data bits which are complementary to data bits of a second portion of said second digital signal when a crash has not occurred;

alternately entering said first and second digital signals into a register and reading contents of said register,

generating an air bag ignition signal when a signal generated by alternately reading said first portions of said first and second digital signals generates an output having a first predetermined frequency.

11. An air bag apparatus comprising:

a crash sensor for sensing existence of a condition indicative that a crash may have occurred;

and air bag igniter;

a control module containing a data processor and a memory;

an abnormality indictor apparatus;

said data processor comprising means for continuously performing a self diagnostic function for detecting a failure in at least the data processor and the memory when no signal is received from said sensor, and for transmitting an abnormality signal to said abnormality indicator apparatus when a failure is detected; and

said data processor further comprising means for interrupting operation of said self diagnostic function when a signal is received from said crash sensor and for performing a crash discrimination function during said interruption, to determine whether a crash has occurred;

wherein said means for continuously performing a self-diagnostic function comprises a plurality of different versions of a self-diagnostic program;

wherein said means for interrupting and for performing a crash discrimination function comprises a plurality of different versions of a crash discrimination program;

wherein said abnormality signal is generated in response to a first comparison by said date processor of output results among said plurality of self diagnostic programs; and

wherein an air bag operation signal is generated in response to a second comparison by said data processor of results among said plurality of crash discriminating programs.

12. Apparatus according to claim 11 wherein results of said first and second comparisons are transmitted to a frequency logic fail-safe circuit.

13. Apparatus according to claim 12, wherein outputs of said data processor are transmitted to said frequency logic fail-safe circuit in the form of alternating signals of predetermined frequency.

14. Apparatus according to claim 13, wherein, when alternating signals are no longer output from said CPU module, or when the alternating signals having a frequency other than said predetermined frequency are transmitted, said frequency logic fail-safe circuit fixes signals transmitted to the air bag device to a value that is necessary for positively inhibiting inflation operation of the air bag.

15. Apparatus according to claim 14, wherein, when alternating signals are no longer output from said CPU module, or when the alternating signals having a frequency other than said predetermined frequency are transmitted, said frequency logic fail-safe circuit fixes signals fed to said abnormality alarm device to a value that is necessary for effecting the abnormality display operation.

16. A method of operating an air bag apparatus having an acceleration sensor, an air bag igniter, and a control means for outputting an operation signal to said air bag igniter, said method comprising the steps of:

generating a signal comprising a mixture of a first signal containing a first signal pattern indicating existence of a normal condition when a self diagnosis of said control means reveals a normal operating condition, and a second signal for operating said air bag igniting apparatus by means of a second signal pattern; and

outputting a signal indicating a failure of said control means in response to detection of a signal other than at least the first signal pattern and the second signal pattern.

17. A method of operating an air bag apparatus having an acceleration sensor, an air bag igniter, and a control means for outputting an operation signal to said air bag igniter, said method comprising the steps of:

performing a self diagnosis to detect a failure of said control means;

generating an interruption signal depending on an output from said control means;

outputting an operation signal to the air bag igniting apparatus in response to said interruption signal;

generating a signal indicating an abnormal condition when the self diagnosis of the control means reveals a failure;

generating a signal comprising a mixture of a first signal containing a first signal pattern indicating existence of a normal condition when a self diagnosis of said control means reveals a normal condition, and a second signal for operating said air bag igniting apparatus by means of a second signal pattern; and

outputting a signal indicating a failure of said control means in response to detection of a signal other than at least the first signal pattern and the second signal pattern.

18. A method of operating an air bag apparatus having an air bag igniter, an electric power source, an acceleration sensor, an abnormality alarm display, and a control means for outputting an operation signal to said air bag igniter, said method comprising the steps of:

performing a diagnosis to detect failures of said acceleration sensor, said air bag igniter, said abnormality alarm display, and said electric power source;

performing a self diagnosis to detect a failure of said control means;

generating an interruption signal depending on an output from said control means;

outputting an operation signal to the air bag igniting apparatus in response to said interruption signal;

generating a signal indicating an abnormal condition when at least one of the diagnoses of said sensor, said air bag igniter, said abnormality alarm display, said electric power source, and the self diagnosis of said control means, reveals a failure;

generating a signal comprising a mixture of a first signal containing a first signal pattern indicating existence of a normal condition when a self diagnosis of said control means reveals a normal condition, and a second signal for operating said air bag igniting apparatus by means of a second signal pattern; and

outputting a signal indicating a failure of said control means in response to detection of a signal other than at least the first signal pattern and the second signal pattern.

19. A method of operating an air bag apparatus having an acceleration sensor, an air bag igniter, and a control means for outputting an operation signal to said air bag igniter depending on an output from said acceleration sensor, said control means comprising at least a data processor, a memory, and a frequency logic input/output device, said method comprising the steps of:

said data processor transmitting a predetermined signal to said frequency logic input/output device when said acceleration sensor generates an output;

said frequency logic input/output device transmitting an operation signal to said air bag igniting apparatus, based on a content of said signal from said frequency logic input/output device;

said control means performing diagnoses to detect failures of peripheral apparatus comprising said acceleration sensor, said air bag igniter, an abnormality alarm display, and an electric power source, when an output from said acceleration sensor does not exist;

said control means performing a routine self diagnosis to detect a failure thereof;

terminating transmission of said predetermined alternating signal from said processing means to said frequency logic input/output device when at least one of said diagnoses of said control means and said peripheral apparatus reveals a failure; and

transmitting a signal indicating an abnormal condition from said frequency logic input/output device to said abnormal alarm display.

20. A method of operating an air bag apparatus having an acceleration sensor, an air bag igniter, and a control means for outputting an operation signal to said air bag igniter depending on an output from said acceleration sensor, said control means comprising at least a data processor, a memory, and a frequency logic input/output device, said method comprising the steps of:

said data processor transmitting a predetermined signal to said frequency logic input/output device when said acceleration sensor generates an output;

said frequency logic input/output device transmitting an operation signal to said air bag igniting apparatus, based on a content of said signal from said frequency logic input/output device;

said control means performing diagnoses to detect failures of peripheral apparatus comprising said acceleration sensor, said air bag igniter, an abnormality alarm display, and an electric power source, when an output from said acceleration sensor does not exist;

said control means performing a routine self diagnosis to detect a failure thereof;

terminating transmission of said predetermined alternating signal from said processing means to said frequency logic input/output device when at least one of said diagnoses of said control means and said peripheral apparatus reveals a failure;

fixing a characteristic of a signal from said frequency logic input/output device to said air bag igniting apparatus at a value necessary to positively inhibit operation of the air bag in response to said termination of transmission of said predetermined alternating signal; and

fixing a characteristic of a signal from said frequency logic input/output device to said abnormality alarm display at a value necessary to operate said abnormality alarm display in response to said termination of transmission of said predetermined alternating signal.

21. An air bag apparatus comprising:

an acceleration sensor;

an air bag igniter;

a control means for outputting an operation signal to said air bag igniter;

means for generating a signal comprising a mixture of a first signal containing first a signal pattern indicating existence of a normal condition when a self diagnosis of said control reveals a normal condition, and a second signal for operating said air bag igniting apparatus by means of a second signal pattern; and

means for outputting a signal indicating a failure of said control means in response to detection of a signal other than at least the first signal pattern and the second signal pattern.

22. An air bag apparatus comprising:

an acceleration sensor;

an air bag igniter;

a control means for outputting an operation signal to said air bag igniter;

means for performing a self diagnosis to detect a failure of said control means;

means for generating an interruption signal depending on an output from said control means;

means for outputting an operation signal to the air bag igniting apparatus in response to said interruption signal;

means for generating a signal indicating an abnormal condition when the self diagnosis of the control means reveals a failure;

means for generating a signal comprising a mixture of a first signal containing a first signal pattern indicating existence of a normal condition when a self diagnosis of said control means reveals a normal condition, and a second signal for operating said air bag igniting apparatus by means of a second signal pattern; and

means for outputting a signal indicating a failure of said control means in response to detection of a signal other than at least the first signal pattern and the second signal pattern.

23. An air bag apparatus comprising:

an acceleration sensor;

an air bag igniter;

an electric power source;

an abnormality alarm display;

a control for outputting an operation signal to said air bag igniting apparatus;

means of performing diagnoses to detect failures of said acceleration sensor, said air bag igniter, said abnormality alarm display, and said electric power source;

means for performing a self diagnosis to detect a failure of said control;

means for generating an interruption signal depending on an output from said control;

means for outputting an operation signal to the air bag igniting apparatus in response to said interruption signal;

means form generating a signal indicating an abnormal condition when at least one of the diagnoses of said sensor, said air bag igniter, said abnormality alarm display, said electric power source, and the self diagnosis of said control, reveals a failure;

means for generating a signal comprising a mixture of a first signal containing a first signal pattern indicating existence of a normal condition when a self diagnosis of said control reveals a normal condition, and a second signal for operating said air bag igniting apparatus by means of a second signal pattern; and

means for outputting a signal indicating a failure of said control in response to detection of a signal other than at least the first signal pattern and the second signal pattern.

24. An air bag apparatus comprising an acceleration sensor, an air bag igniter, and a control means for outputting an operation signal to said air bag igniter, wherein:

said control means comprises at least a data processor, a memory, and a frequency logic input/output device;

said data processor transmits a predetermined alternating signal to said frequency logic input/output device when said acceleration sensor generates an output, and simultaneously, said frequency logic input/output device transmits an operation signal to said air bag igniter, based on a content of said signal from said frequency logic input/output device;

said control means performs diagnoses to detect failure of peripheral apparatus comprising said acceleration sensor, said air bag igniter, an abnormality alarm display, and an electric power source, and also performs a routine self diagnosis, when an output from said acceleration sensor does not exist; and

said transmission of the predetermined alternating signal from said processing means to said frequency logic input/output device is terminated when at least one of said diagnoses of said control means and said peripheral apparatus reveals a failure, and simultaneously, said frequency logic input/output device transmits a signal indicating an abnormal condition to said abnormality alarm display.

25. An air bag apparatus comprising an acceleration sensor, an air bag igniter, and a control means for outputting an operation signal to said air bag igniter, wherein:

said control means comprises at least a data processor, a memory, and a frequency logic input/output device;

said data processor transmits a predetermined alternating signal to said frequency logic input/output device when said acceleration sensor generates an output, and simultaneously, said frequency logic input/output device transmits an operation signal to said air bag igniter, based on a content of said signal from said frequency logic input/output device;

said control performs diagnoses to detect failure of peripheral apparatus comprising said acceleration sensor, said air bag igniter, an abnormality alarm display, and an electric power source, and also performs a routine self diagnosis, when an output from said acceleration sensor does not exist; and

said transmission of the predetermined alternating signal from said data processor to said frequency logic input/output device is terminated when at least one of said diagnoses of said control and said peripheral apparatus reveals a failure, and simultaneously, a characteristic of a signal which is transmitted from said frequency logic input/output device to said air bag igniter is fixed at a value necessary to positively inhibit operation of the air bag, and a characteristic of a signal from said frequency logic input/output device to said abnormality alarm display is fixed at a value necessary to operate said abnormality alarm display.