SOVEREIGN COMPLIANCE ATLAS

DRDO Avionics :: Fly-By-Wire Quad-Redundant Flight Control

Deterministic systems profiling, Ring-0 IPC transfer rates, and bare-metal microkernel execution verification under the ARKM 12-core SMP operating substrate.

Jitter Bound<30 ns

Ring-0 IPC Cycles94 cycles

Fault BoundaryRing 0 / 3 IPC

Foreign Runtimes0 (Zero Dep)

Real-Time Execution & Hard Determinism

Deterministic actuator servo loop cycling at 1000Hz with zero jitter or preemption drift.

APIC Dispatch Vector: Direct Hardware Inter-Processor Interrupt (Vector 0x20)

Sovereign Mandates & Zero-Telemetry Audit

Guarantees flight-critical fault boundary containment; crash of telemetry HUD never halts flight controls.

Subsystem Register Mapping & Allocation

target:Actuator Control Loop

failover:Immediate

standard:DO-178C DAL-A

framework:DRDO Avionics Standard

Core Architectural MechanismARKM 12-Core Bare-Metal SMP Microkernel

Examine Kernel Teardown→