Electronic module assembly for controlling aircraft restraint systems

1. An electronic module assembly for controlling the deployment of one or more airbags in a vehicle, comprising:

a power source;

a crash sensor configured to produce a signal in response to a crash event;

an accelerometer that is configured to produce a signal in response to a crash event;

a processor configured to receive the signals from the crash sensor and the accelerometer, wherein the processor is configured to:

start a timer upon detection of the signal from the crash sensor;

determine if a signal has been received from the accelerometer indicating the occurrence of the crash event;

if signals from both the crash sensor and the accelerometer indicate a crash event then

read a timing value selected for an inflator in a memory associated with the inflator;

determine if the timer has a value equal to the timing value selected for the inflator; and

produce a signal to fire the inflator when the timer has a value equal to the timing value selected for the inflator.

2. The electronic module assembly of claim 1 , wherein the processor is further configured to:

read a value from the memory associated with the inflator to determine if a status of a seat belt buckle needs to be determined before firing the inflator and if so,

determining the status of the seat belt buckle before producing the signal to fire the inflator.

3. The electronic module assembly of claim 2 , further comprising a seat belt latch detection circuit including:

a circuit to direct power from the power source to a Hall effect sensor;

a comparator for comparing a signal from the Hall effect sensor against a known voltage to determine if a seat belt buckle is latched;

wherein the processor is configured to control when the latch detection circuit delivers power to the Hall effect sensor and when the comparator is powered to determine if the seat belt buckle is latched.

4. The electronic module assembly of claim 3 , wherein the circuit for directing power to the Hall effect sensor and the comparator are connected to an intermediate ground and the processor is configured to connect the intermediate ground to a ground shared by the power source of the electronic module assembly in order to direct power to the Hall effect sensor and to power the comparator.

5. The electronic module assembly of claim 1 , further comprising a relay that is set to provide power to an inflator by a signal from the crash sensor.

6. The electronic module assembly of claim 5 , further comprising a transistor in series with the inflator that is controlled by the processor to complete a current path from the relay and though the inflator in order to fire the inflator.

7. The electronic module assembly of claim 5 , wherein the relay is configured to apply a voltage to the inflator having a value that is not great enough to fire the inflator and the transistor that fires the inflator is bypassed with a resistor, wherein the processor is configured to read a voltage at the bypassing resistor when the voltage applied to the inflator is not great enough to fire the inflator is in order to determine if the inflator is operable.

8. The electronic module assembly of claim 1 , wherein the power source includes one or more batteries, further comprising:

a power source testing circuit that is controlled by the processor to place a load on the one or more batteries and to read a voltage produced by the batteries when under the load.

9. The electronic module assembly of claim 1 , wherein the accelerometer is coupled to resistor/capacitor circuit that is charged when the accelerometer subjected to a crash event in order to produce the signal in response to the crash event.