Hi, i always had the question on how to manage a complete failure of Flight Control systems
i kow some implementations on extra procesors asisted systems are implemented in a great group
of modern and old flight controllers.
So for example, i think its interesting have 2 FC in the same structure, so if one is ded the other one
continues....thats already implemented on pixhawk in a diferent way
so with the schematic "B" we have 2 pixhawk with one gps..
so in that way we have an optocopter with 2 pixhawks...
It apears to be that Ardupilot Software dont use the co-processor of the pixhawk system..
So, i would like to know more abut that...
Ardupilot really uses the Co-procesor in case the principal fails,?or not...
thanks a lot for comment..