SecureEvtol: Zero-Trust Avionics & Cryptographic Flight Control Links
SecureEvtol establishes zero-trust cybersecurity architectures for electric vertical takeoff aircraft, binding flight control actuators, battery management computers, and fly-by-wire flight control computers through hardware roots of trust, mutual TLS 1.3, and anti-tamper silicon enclaves.
SecureEvtol Zero-Trust Avionics Control Bus & Cryptographic Enclave Architecture
Mutual TLS 1.3 micro-bus, hardware security chip attestation, and anti-tamper cryptographic vault
Central System: Zero-Trust Flight Controller - Mutual TLS 1.3 & Attestation Engine
Aviation Architecture Nodes
- Hardware Cryptographic Root of Trust
- Cryptographic Actuator Drive Node
- Battery Management Enclave (BMS)
- Dual-Key Maintenance Authorization Port
- Tamper-Proof Flight Recorder Vault
Architectural Layers & Protocol Stacks
- Hardware Silicon Security & Key Enclaves (Hardware Security Module (HSM) / Secure Enclaves): Anchoring cryptographic identities in physical silicon; private keys can never be extracted even under physical decapping attacks.
- Internal Bus Mutual Cryptographic Attestation (Mutual TLS 1.3 over CAN FD / Micro-mTLS): Authenticating every single motor speed command and flight surface deflection with microsecond cryptographic handshakes.
- Battery Management & Telemetry Integrity (HMAC-SHA256 Signed Telemetry Channels): Ensuring battery thermal readings and cell voltages cannot be spoofed to conceal impending thermal runaway.
- Airworthiness Maintenance Cryptographic Keys (Two-Man Rule Dual Cryptographic Sign-Off): Requiring dual cryptographic keys from certified A&P mechanics and safety officers before authorizing maintenance firmware flashes.
Flight Telemetry Metrics: 100% (Actuator Command Cryptographic Verification) | < 50 µs (Hardware Micro-mTLS Authentication Latency) | FIPS 140-3 (Silicon Root-of-Trust Rating) | Zero Trust (Internal Avionics Architecture)
Cryptographically Enforced eVTOL Control Links, Zero-Trust Avionics & Hardware Root of Trust
Authoritative technical engineering reference for cryptographically enforced evtol control links, zero-trust avionics & hardware root of trust in FAA Part 135/27, DO-178C DAL A avionics software, DO-254 hardware, 4D trajectory deconfliction, and ASTM F3411 Remote ID.
Core Engineering Areas
Technical Publications
Related Cluster Architecture Specifications
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