AVERY CORE KINETICS // PRE-GOVERNED HYBRID AI STACK

AI-04 // FLIGHT-AERO™

Bind autonomous flight perception and planning to a DO-254-oriented hardware interposer that overrides invalid navigation and flight-surface vectors independently of the AI runtime.

HYBRID STACK = OPEN AUTONOMOUS FLIGHT VLA / MULTIMODAL PLANNER + BASE GOVERNANCE (ASSETS 1–4) + AI-04 FLIGHT-AERO™ VHDL SOFT IP + [PROTECTED BY ASSETS 65–69]

MODEL & VISION ENCLOSURE

Integration targets include open vision-action and multimodal planning models for UAV and autonomous flight research
INT8 / FP16 inference with EO/IR, radar, inertial, GNSS, terrain, and mission-context encoder pipelines
Model paths are quantized into bounded heading, altitude, airspeed, route, and actuator command descriptors
MIL-STD-1553, ARINC 429, SpaceWire, CAN Aerospace, and AXI4 flight-control registers stay hardware isolated

BARE-METAL VETO FLOOR

Flight-envelope, geofence, altitude, bank-angle, actuator-rate, or control-surface position violation
GNSS/inertial divergence, stale sensor timestamp, impossible route transition, or spoofed source identity
Illegal 1553 command, ARINC label mismatch, bus-controller takeover, or fallback-controller disagreement
Watchdog loss, single-event upset, clock/reset fault, or radiation-induced state error forces deterministic fallback

VHDL SOFT IP ARCHITECTURE

Radiation-tolerant VHDL-2008 interposer separates NPU planning output from certified flight-control register paths
Redundant sensor comparators and optional TMR policy state maintain authority outside the model accelerator
DO-254 Level A-oriented requirements trace model commands to bounded hardware acceptance and override outputs
Six-domain target with 12–28 cycle verdict, sub-2.8µs surface inhibit, TMR path groups, and constrained I/O budgets

— DOMAIN DEPLOYMENT CASES // AVIONICS, SPATIAL FLIGHT & AUTONOMOUS UAV —

01Tactical UAV rejecting model-generated paths that violate geofence or flight-envelope limits
02Collaborative aircraft transferring compromised AI control to a wired fallback controller
03Autonomous cargo aircraft bounding approach and control-surface commands at the avionics bus
04Space vehicle isolating AI attitude-control requests before SpaceWire and reaction-wheel release

MODEL WEIGHTS REMAIN CUSTOMER-SELECTED · SUB-2.8µs TARGET REQUIRES DEVICE-SPECIFIC TIMING CLOSURE

EVALUATE AI-04 HYBRID STACK ON BENCH REQUEST WHOLESALE AI-04 LICENSING

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