Blindaje Fly-by-Wire con Triple Redundancia para Movilidad Aérea Urbana
eVTOLShield garantiza una estabilidad absoluta de control de vuelo para aeronaves multirrotor y de ala basculante, aislando al instante fallos en motores, amortiguando turbulencias y previniendo la pérdida de control bajo normas FAA 10^-9.
eVTOLShield Triple-Modular Redundant Architecture
Tri-Channel Voting, High-Bandwidth Actuator Bus & Real-Time Thrust Allocation
Central System: Tri-Channel Voter & Control Executive - 2-out-of-3 Fault Elimination Core
Aviation Architecture Nodes
- Channel A: Primary Compute Node
- Channel B: Dissimilar Compute Node
- Channel C: Backup Fallback Core
- Direct Rotor Inverter H-Bridge Gate
- Triplicated IMU & Air Data Sensors
Architectural Layers & Protocol Stacks
- Tri-Channel Voting & Hardware Dissimilarity (DO-254 DAL A Dissimilar Silicon / TMR Hardware Voter): Three independent flight computers running 2-out-of-3 bitwise voting, utilizing dissimilar microprocessors to eliminate common-cause silicon bugs.
- Instantaneous Rotor Failure Accommodation (Dynamic Control Allocation / Quadratic Programming Solver): Control allocation algorithms that redistribute rotational torque and lift across healthy rotors within 5ms of an inverter or motor loss.
- Hard Flight Envelope Protection Limits (Control Barrier Functions / Certified Invariant Envelopes): Mathematical barrier functions preventing pilot inputs or automated autopilots from exceeding maximum bank angles, pitch attitudes, or G-loads.
- Electromagnetic & Lightning Surge Shielding (RTCA DO-160G Section 22 Level 5 Lightning Hardening): Rugged galvanic isolation, optical sensor coupling, and surge arrestors certified against direct lightning strikes under DO-160G Section 22.
Flight Telemetry Metrics: < 5 ms (Rotor Failure Isolation & Re-trim Latency) | 10^-9 (Probability of Catastrophic In-Flight Loss) | DAL A (DO-254 and DO-178C Certification Level) | 100% (Aerodynamic Departure Prevention Rate)
Acomodación de Fallo Catastrófico a 300 Metros de Altitud
Unlike conventional airliners with aerodynamic gliding capability, multi-rotor eVTOLs rely entirely on continuous thrust to stay airborne. eVTOLShield deploys triple-modular redundant (TMR) flight control computers that detect motor failures in less than 5 milliseconds, dynamically redistributing thrust across remaining rotors to maintain stable, level flight.
Core Engineering Areas
- Triple-Modular Redundancy — Eliminating single points of failure through hardware voting, synchronized clock domains, and dissimilar microcontrollers.
- Rotor Fault Accommodation — Preserving vehicle control and safe landing capability following the sudden loss of an electric motor.
- Envelope Protection — Software and hardware limiters that mathematically prevent pilots or automated systems from overstressing the airframe.
Technical Publications
Related Cluster Architecture Specifications
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- AAVDelivery — Autonomous Aerial Vehicle (AAV) Last-Mile Delivery, Automated Tethered Winch Drops & Urban Parcel Logistics
- AAVPort — Automated Vertiport Infrastructure, Final Approach Guidance & Megawatt eVTOL Fast-Charging
- AAVSwarm — Autonomous Cargo Drone Swarms, Distributed Consensus & Mesh Formation Flight