Triple-Modular Redundant (TMR) Fly-by-Wire Architecture for eVTOL

Eliminating single points of failure through hardware voting, synchronized clock domains, and dissimilar microcontrollers.

2-out-of-3 Hardware Majority Voting

Three independent flight control computers process identical sensor streams in lockstep. An analog and digital voting circuit compares actuator commands; if one channel deviates, it is silently disconnected while the remaining two maintain seamless flight guidance.

Hardware Dissimilarity Against Common-Cause Faults

To protect against obscure microcode flaws or silicon errata, Channel A uses ARM Cortex-R real-time cores while Channel B executes on RISC-V, guaranteeing that a hardware-level processor bug cannot crash all redundant lanes simultaneously.

Aerospace-Domains ansehen