Dynamis
Engine 05 / 05 · Avionics & Embedded · Independent
Avionics resolved to closed budgets —
every margin stated and every fault path argued.
Explore more ↓ELECTRONICS AND INTEGRATION
Avionics architecture, budgeted and bounded
Avionics architecture
Federated or integrated — redundancy schemes, bus topologies, and partitioning with the trade recorded.
Interface control documents
ICDs drafted and kept consistent — signals, connectors, protocols, timing.
Power & signal budgets
Bus loading, worst-case draw, derating, and margin — per EEE-INST-002-class discipline.
Hardware compliance
DO-160 environmental categories and DO-254 hardware assurance mapped to your design.
Fault tolerance & FMEA
Failure modes, detection coverage, and single-failure tolerance argued explicitly.
A WORKED ARTIFACT
Budgets that close, with margin declared
DYNAMIS reports the governing envelope, the load accounting, the derived margin, and the fault-tolerance argument — figures an integrator can verify against the hardware.
BUS 28 V DC primary · MIL-STD-704F envelope
LOADS FCC 18 W · IMU 9 W · radio 31 W (44 W peak) · heaters 22 W
DERIVE steady 80 W · worst-case 116 W · source rating 160 W
MARGIN worst-case margin 27 % · closes ✓ · derating per EEE-INST-002
FAULT single-failure tolerant · dual FCC supplies, diode-OR'd
VERIFIED · TRACEABLE TO FIRST PRINCIPLES
ACROSS THE SUITE
Independent by design
No pipeline connects them. Engage the engine your task requires, in any order.
DYNAMIS · AEROSPACE INTELLIGENCE