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Avionics & Flight Systems

Integrated flight control architectures, sensor fusion platforms, and cockpit management systems engineered for high-reliability aerospace platforms. From MIL-spec UAS to commercial next-gen aircraft, our avionics solutions deliver deterministic performance, redundant safety margins, and seamless mission-system integration.

Core Capabilities

Flight Control Computers (FCC)

Triple-modular redundant (TMR) flight control processors with real-time deterministic scheduling, fault-tolerant architecture, and adaptive control law implementation.

ARINC 653 / POSIX RT

Sensor Fusion & Navigation

Multi-sensor inertial navigation systems (INS/GPS/DSPS) with extended Kalman filtering, aiding source validation, and anti-jam/spoofing countermeasures.

MEMS/FOG / GNSS-III

Cockpit Integration & Displays

Modular cockpit ecosystems featuring HUD, HMD, MFD, and EICAS integration with standardized data bus routing and pilot workload optimization protocols.

DO-229 / ARINC 661

Data Link & Communications

Secure mission networking, waveform management, and cross-domain data exchange supporting Link 16, MADL, and commercial SATCOM/VHF protocols.

MIL-STD-1553B / 1815B

Avionics Cybersecurity

Hardware-rooted trust, cryptographic key management, intrusion detection systems (IDS), and secure boot chains compliant with modern defense cybersecurity mandates.

RMF / Zero-Trust Arch

Ruggedization & Environmental

Conduction-cooled, shock/vibration resilient enclosures rated for extreme thermal cycling, altitude, and electromagnetic compatibility (EMC/EMI) environments.

MIL-STD-810 / 461

System Architecture

Our avionics framework follows a modular open systems approach (MOSA), enabling rapid technology insertion and cross-platform compatibility while maintaining strict real-time performance guarantees.

Flight Sensors

AOA / AOS / Pitot / IMU

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Signal Conditioning

Analog-to-Digital / Filtering

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FCC Cluster

TMR Processing / Control Laws

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Actuation & EFB

Servo Drives / Flight Controls

Technical Specifications

Parameter AV-X1 FCC Platform AV-S2 Sensor Hub AV-D4 Display Module Development Status
Processing Architecture Dual PPC 750 / PowerPC e500 ARM Cortex-R52 (Lockstep) Xilinx Zynq Ultrascale+ ● Production
Real-Time OS VxWorks 6.9 / INTEGRITY FreeRTOS / SafeRTOS Linux RT / ARINC 653 ● Production
Data Bus Interfaces MIL-STD-1553B, ARINC 429, Ethernet ARINC 429, CAN, RS-422 MIL-STD-1553B, ARINC 664 ● Production
Redundancy Config 2oo3 Voting / Hot-Hot-Hot Diverse Dual-Redundant Dual-Channel Failover ● Production
Thermal Range -55°C to +71°C -40°C to +85°C -40°C to +70°C ● In Validation
EMC/EMI Class MIL-STD-461G (CE102, RE102, CS114) MIL-STD-461G / DO-160G Sec 20 DO-160G / FCC Part 15 ● Certified

Standards & Certification

All avionics hardware and software development lifecycle processes are aligned with international aerospace safety and assurance standards. Full traceability, verification, and validation packages provided.

✓
DO-178C (DAL A-C)
✓
DO-254 (ASIL/ DAL)
✓
RTCA DO-326A (Cyber)
✓
DO-338 (Software Tool)
✓
MIL-STD-810H (Env)
✓
AS9100D / ISO 9001
✓
ITAR / EAR Compliant

Request Technical Documentation

For integration guides, block diagrams, interface control documents (ICDs), or capability briefings, submit a technical inquiry through our secure engineering portal.