Problems with the Dreamliner battery

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donpacino said:
A few things to consider about aircraft control computers.
There are independently reset-able paths usually using dissimilar hardware. Resetting a CPU or event an entire board will barely effect system operation.

Most electrical systems on a modern airplane reset once or twice a flight due to single event upsets (SEUs).

Very interesting. In this context when you talk about an electric system resetting itself what is the smallest resettable unit? e.g. when a SEU happens how large is the system that gets reset?

Or when you talk about resetting a Dreamliner CPU, how many CPUs are on board in the first place?
 
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rollingstein said:
Very interesting. In this context when you talk about an electric system resetting itself what is the smallest resettable unit? e.g. when a SEU happens how large is the system that gets reset?

Or when you talk about resetting a Dreamliner CPU, how many CPUs are on board in the first place?

So a single flight computer system is typically made up of multiple boards. You can typically reset on a box (multiple boards), board(multiple functions), or function level. examples of functions are com channels, watchdog channels, and flight mode channels. You can sometimes even reset individual memory blocks (which will most likely disable that entire function for that frame). I would say the smallest electronic system you can reset is a function.

I don't know the dreamliner's architecture, but think of it this way. If there are 3 redundant paths in each computer, and you have say 8 actuators computers, 2 mission/flight computer, at a minimum you'll have 30 flight critical cpus. I would say that's a LOW estimate.
 
donpacino said:
You can typically reset on a box (multiple boards), board(multiple functions), or function level.

box & board resets I can understand but what does a function level reset mean? Or even a memory reset. i.e. If you reset memory how do you get a coherent state for the OS wherever it was last before the reset? Ditto for a function reset. A function is a software entity right? So this would be a soft reset?
 
rollingstein said:
box & board resets I can understand but what does a function level reset mean? Or even a memory reset. i.e. If you reset memory how do you get a coherent state for the OS wherever it was last before the reset? Ditto for a function reset. A function is a software entity right? So this would be a soft reset?
I shouldn't have used the word function. By function I meant a 'block' or a circuit that preforms a particular task. An example of this is on a typical PC if you had the ability to reset the hardware (not the software) of an individual usb port.

with the memory reset issue you may need to restart the OS or some higher level function depending on what part of memory was affected. In flight critical applications all or most memory is partitioned for specific use. Even then, the reset times for most systems are not that long (hard resets are anywhere from 10 ms to 200 ms). software can be much longer (seconds). But compared to windows operating systems, its blazing fast
 
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Are the single event upsets so much more often due to the altitude of flights & related increase in energetic particle bombardment?
 
rollingstein said:
Are the single event upsets so much more often due to the altitude of flights & related increase in energetic particle bombardment?
I don't know that much about SEUs. I know what they are. I know how they effect electronics. I know that the thinner the atmosphere, the more prevalent they are.
 
donpacino said:
I don't know that much about SEUs. I know what they are. I know how they effect electronics. I know that the thinner the atmosphere, the more prevalent they are.

How come they don't cause laptops or similar electronic devices that have no special protection against SEUs to keep crashing when used on aircraft?
 
rollingstein said:
How come they don't cause laptops or similar electronic devices that have no special protection against SEUs to keep crashing when used on aircraft?

The sensors, wiring and interfaces are exposed to high energy transients from power control activators and hull discharges from static. A person sitting at a seat is usually well shielded by the cabin and are far away from most EMI/ESD sources.