RRH covers AW2S Remote Radio Head and Remote Radio Unit platforms used in modern wireless infrastructure. AW2S designs radio equipment spanning 2G through 5G and combines those products into private, tactical, professional-mobile-radio and cellular network solutions. Moving the radio function close to the antenna can reduce feeder losses and support distributed base-station architectures, while the selected radio unit determines bands, output power and supported access technology. SERMA Ingénierie also identifies RF transmit/receive and remote-radio-head development within its telecommunications activities. Exact band combinations, power classes, cooling and fronthaul interfaces depend on the chosen AW2S configuration.

Key capabilities

• Remote radio head and remote radio unit architecture
• Support across documented 2G-to-5G product families
• Private, tactical, PMR and cellular deployment options
• RF transmit and receive functions close to the antenna
• Configurable bands, power and network integration

Typical applications

Private mobile networks, tactical communications, PMR coverage, cellular infrastructure and coverage-extension deployments.

LFR is a Lightweight Flight Recorder concept aimed at aircraft where mass, volume and installation complexity must be tightly controlled. The published product information combines flight data, audio and 4K video recording with integrated microphone, GNSS and inertial sensing functions. The crash-protected design references the ED-155 minimum operational performance standard for lightweight recording systems. SERMA Ingénierie’s BANKSIA research program also confirms ongoing work on an ultra-compact ED-155 recorder for light aviation and future air-mobility applications. Final qualification, recording duration, interface set and production configuration remain program dependent and should be confirmed against the latest approved datasheet.

Key capabilities

• Combined aircraft data, audio and video recording
• Integrated microphone, GNSS and inertial sensors
• Compact lightweight architecture
• 4K HDR video capability in the documented concept
• Crash-protection objectives aligned with ED-155 lightweight recorders

Typical applications

Light aircraft, rotorcraft, unmanned platforms and emerging air-mobility vehicles requiring compact flight-data recording.

Verified specifications

• Documented mass: Approximately 800 g
• Video: Integrated 4K HDR in the documented concept
• Reference standard: ED-155

MIB 5 is described as a Mission Board Interface for coordinating selected mission-system functions on an aircraft. The current record identifies sonar management and fast-rope management among its roles, placing the unit between operator or mission commands and the connected subsystems. It is also associated with a high-assurance hardware development environment. SERMA Ingénierie’s current portfolio confirms build-to-spec embedded electronic equipment and experience with high-criticality aeronautical systems, but no public model-specific datasheet is available. For that reason, the page avoids claims about platform, processor, interfaces, redundancy or certification and presents only the consistently documented functional scope.

Key capabilities

• Mission-board interface and subsystem coordination
• Sonar-management interface functions
• Fast-rope system management functions
• Embedded operation in demanding aircraft environments
• High-assurance hardware development context

Typical applications

Mission-system integration on specialized aircraft requiring controlled interfaces to sonar or fast-rope subsystems.

RDC is a Remote Data Concentrator intended to collect distributed aircraft signals and consolidate them for the wider avionics system. The published record describes separate channel-A and channel-B architecture and an ASIC-based design developed for a high-reliability embedded environment. It also identifies a mixed input and output role, allowing the equipment to reduce point-to-point wiring between remote aircraft functions and central computers. SERMA Ingénierie’s current aeronautical portfolio confirms its work on embedded electronic equipment, FPGA and safety-critical developments. Public model-specific documentation is limited, so interface standards, I/O electrical characteristics, redundancy behaviour and qualification levels are left unspecified.

Key capabilities

• Remote concentration of distributed aircraft data
• Separate channel-A and channel-B architecture
• Mixed input and output handling
• ASIC-based embedded implementation
• Designed for high-reliability avionics integration

Typical applications

Distributed aircraft I/O collection and wiring consolidation between remote equipment and central avionics computers.

Verified specifications

• Documented I/O: 59 inputs and 22 outputs
• Architecture: Channel A / Channel B

ASU is presented as an Ancillary System Unit computer for embedded aircraft architectures. Its principal role is to concentrate data acquired through avionics interfaces such as ARINC 429 and CAN, then de-format and translate that information for other aircraft functions. The existing product record also identifies controlled management functions implemented in hardware and software intended for a safety-critical environment. SERMA Ingénierie’s current portfolio confirms its work on build-to-spec embedded electronic equipment, data interfaces and high-criticality aeronautical developments. Because a current public model-specific datasheet is not available, no processor, channel-count, environmental or certification value is claimed beyond the documented functional role.

Key capabilities

• Concentration of data from aircraft avionics interfaces
• ARINC 429 and CAN data acquisition
• De-formatting and translation between bus data and aircraft interfaces
• Embedded hardware and software management functions
• Designed for integration into safety-critical avionics architectures

Typical applications

Aircraft data concentration and interface-management functions in customized embedded avionics systems.

CVC is an embedded Cockpit Video Camera intended to capture and manage video within an aircraft environment. The published functional description combines image compression, onboard recording, removable memory and Ethernet streaming in a compact Linux-based architecture. These functions allow cockpit imagery to be stored locally while also being shared with another onboard system when the aircraft integration supports it. SERMA Ingénierie’s current aeronautical portfolio shows camera and embedded-equipment work alongside build-to-spec electronics for constrained environments. Public sources do not provide a current model-specific resolution, frame rate, interface speed or qualification level, so those values must be confirmed for the project configuration.

Key capabilities

• Cockpit video capture
• Onboard image compression and recording
• Removable recording media
• Ethernet video streaming
• Embedded Linux processing architecture

Typical applications

Cockpit monitoring, mission review, test recording and integration with aircraft video-distribution systems.

FCSAU is a Flight Control System Auxiliary Unit used within a helicopter’s wider flight-control architecture. The available product record identifies interfaces to the Primary Flight Control System and Automatic Flight Control System, crew interaction and trim-release management. Independent NH90 technical documentation also identifies an FCSAU as part of the primary flight-control system and associates it with flight-control reconfiguration needs. SERMA Ingénierie’s aeronautical portfolio includes an FCSAU equipment example and confirms experience with high-criticality embedded electronics. The unit is described only at functional level; internal redundancy, channel count, software baseline and qualification status depend on the aircraft program and approved configuration.

Key capabilities

• Interface support for primary flight-control functions
• Interface support for automatic flight-control functions
• Crew interaction within the flight-control architecture
• Trim-release management
• Flight-control reconfiguration support in documented helicopter architecture

Typical applications

Auxiliary control and crew-interface functions within redundant helicopter primary and automatic flight-control systems.

EVC is an External Video Camera developed for integration into airborne video architectures. The available product description identifies four principal functions: supporting pilot-assistance displays, providing imagery for flight operations, recording external views and supplying video for entertainment or mission systems. SERMA Ingénierie’s current aeronautical portfolio includes an external-camera example alongside its embedded electronic equipment and build-to-spec capabilities. The camera is therefore presented as an integration component rather than a standalone consumer-imaging device. A current public model-specific datasheet is not available, so resolution, optical field of view, environmental qualification, interface type and enclosure performance are intentionally left configuration dependent.

Key capabilities

• External airborne video capture
• Video feed for pilot-assistance displays
• Operational and flight-recording support
• Integration with aircraft entertainment or mission-video systems
• Build-to-spec embedded-aircraft integration

Typical applications

Aircraft external-view monitoring, pilot assistance, flight recording and mission or cabin video distribution.