Twin-Motor Fixed-Wing UAV
Avionics Integration Digital Twin
Review-oriented web package for the aircraft power system, flight-control architecture, mission computer, communications, sensors, harness, software interfaces and fail-safe logic. Structural and flight-science interfaces remain visible, but this release intentionally prioritizes Avionics & Software.
3D Avionics Architecture & State Simulation
Click equipment in 3D or in a table to inspect it
System State Demonstration
Normal mode animates both propellers, power flow and data packets. Termination mode demonstrates the approved command/state behavior for RC-loss fail-safe: thrust cut and left/down descending spiral visualization.
2D Power + Data Architecture
Click any node to jump to its 3D location
Power Budget & Rail Margin
Known energy values + explicit open verification items
Interface Control Matrix
Source → destination → electrical/data interface → criticality
| Source | Destination | Interface | Role | Domain | Criticality |
|---|
Equipment Master List
Model, quantity, size, mass, location and interface
| System | Component | Model | Qty | Dimensions | Unit mass | Total mass | Installation | Interface |
|---|
Harness, Connectors & 3D Routing
Workbook connector schedule and 3D route estimate are deliberately separated
| # | Connection | Cable / AWG | Cond. | g/m | Length | Connector A | A g | Connector B | B g | Current subtotal |
|---|
Fail-Safe & Degraded-Mode Register
Baseline requirements are separated from proposed handling
Avionics Requirement Traceability
44 avionics TLARs extracted from the team workbook
| Requirement | Category | English text | Method of Compliance | Status |
|---|
Engineering Issues, Assumptions & Source Control
Conflicts are visible rather than silently corrected