Avionics and Navigation Systems

ACORE GB establishes data and communication interfaces with MXF-484 and 9681 V/UHF Airborne Radio, MILSEC-3 Secure Voice Device, EO/IR Sensor Suite, SAR Radar, Airborne Data Terminal Communication Unit along with the mission software of the ANKA UAV.

ACORE HUMS is a sensor-based monitoring system that enables Condition-Based Maintenance by measuring the health and performance of missioncritical components in rotary wing aircraft.

ACORE MGB, Advanced Modular Computer, is the processing center of the Integrated Fighter Avionics System. ACORE MGB is based on multiple, high performance quadcore PowerPC family processors.

ACORE MKB Central Control Computer is the key for mission success. ACORE MKB is the mission computer which manages avionics, supports pilot with its advance processing capability, and provides relevant data to the pilot collected from aircraft systems.

Integrated Central Control Computer (ACORE TMKB) is the central control computer of the aircraft that manages avionics and reduces the workload of pilot with its advance processing capability.

ADAC 400 and 500 (Air Data Unit) is a configurable air data unit designed and developed by ASELSAN. It can be used as primary air data source for various aircraft systems.

ADEN CCD 68 Central Cockpit Display is designed as color flat panel display using Active Matrix Liquid Crystal Display (AMLCD) technology, with an active display area of 6 by 8 inches.

ADEN CMFD 55 Color Multifunciton Display is designed as color flat panel display using Active Matrix Liquid Crystal Display (AMLCD) technology, with an active display area of 5 by 5 inches.

With its compact, platform-configurable and user-friendly design; Engine Instrument Display (ADEN EID) meets the customer needs and platform requirements by displaying platform critical engine data.

With its compact, platform-configurable and user-friendly design; Fuel Hydraulic Display (ADEN FHD) meets the customer needs and platform requirements by critical fuel quantities, hydraulic pressure data and fuel balance/imbalance status.

ADEN GMFD 68 smart multifunctional display is designed by ASELSAN to generate graphical operator interface and to be used in digital map applications by processing data provided by external avionics.

ADEN IMD 820 controls the avionics systems and generates flight/mission graphics and performs video overlays onto a dual redundant, separately addressable, two left and right 1280x1024 resolution half displays via one 2560x1024 resolution AMLCD.

ADEN KDU 44 Keyboard Display Unit is a color display using Active Matrix Liquid Crystal Display (AMLCD) technology, with an active display area of 4 by 4 inches.

The ADEN KDU 45 Keyboard Display Unit has a color display based on Active Matrix Liquid Crystal Display (AMLCD) technology with an active display area of 4 by 5 inches.

Super Multifunction Display (SMFD-810) is a multifunctional display which operates as a mission computer and display system packaged into one Line Replaceable Unit (LRU).

Touchscreen Cockpit Control Unit (ADEN TCCU 810) is a primary cockpit control interface between the pilot and the aircraft. ADEN TCCU 810 is a Line Replaceable Unit (LRU) which provides display and control of subsystems and interfaces of aircraft for pilot.

VMFD-68 Multifunciton Display is designed as color flat panel display using Active Matrix Liquid Crystal Display (AMLCD) technology, with an active display area of 6 by 8 inches. It is specially designed for mission computer applications with analog/digital video input displaying and digital input/output processing capabilities.

ADEN VMFD 810 Multifunction Display is designed as color flat panel display using Active Matrix Liquid Crystal Display (AMLCD) technology, with an active display area of 8 by 10 inches. It is specially designed for mission computer applications with digital video input displaying and digital input/output processing capabilities.

AICON DHS 101 is an analog Intercommunication System (ICS). The System provides communication between pilot and co-pilot, communication equipment management and integrating audio and intercom facilities together with all audio caution and warning messages.

AICON DHS 121 is an analog Intercommunication System (ICS). The System provides communication between pilot and co-pilot, communication equipment management and integrating audio and intercom facilities ah all audio caution and warning messages.

AICON DHS 201 is a Digital Intercommunication Systems (ICS). The System provides communication between aircraft crewmembers, managing communication equipments, and integrating audio and intercom facilities together with all audio caution and warning messages.

AICON DHS 300 manages airborne radios, receivers and units with voice alerts and also provides communication interface for pilot and copilot.

AMAC ADCP is an avionic control panel designed to provide Man Machine Interface (MMI) for the following functions.
- Barometric Setting
- Course Selection
- Radar Altitude High Setting
- Radar Altitude Low Setting
- Zeroize
- Emergency Transponder Activation
- Communication Emergency
- Emergency Reset

AMAC MFSC is a control unit designed by ASELSAN to control cursor movement on displays. AMAC MFSC is ergonomically designed to control cursor movement on the displays for the Pilot and Copilot.

Main responsibility of AMAC MGRIP is to provide user interface for weapon systems, targeting system, digital moving map and multi functional displays.

Multi-Functional System Controller (AMAC MSC) is an avionic control panel designed by ASELSAN to control cursor movement on displays.

Master Warning / Caution Panel consists of two independent indicators for the annunciation to the pilot and copilot. Master Caution Rectangular Illuminated Indicator is responsible of indicating/resetting caution situations to pilot and copilot via illuminated buttons. Master Warning Rectangular Illuminated Indicator is responsible of indicating/resetting warning situations to pilot and copilot via illuminated buttons.

AMAC UFCP is specially designed to enable the pilots to control the A/C systems using pushbuttons, rotary knobs, rocker switch and joystick. AMAC UFCP includes potentiometers which provides additional controls related with the HUD operation. AMAC UFCP includes a yellow-green dot matrix LED display to provide annunciation and warning functions to the pilots.

ARAL is a Line Replaceable Unit (LRU) which provides the aircraft clearance over the over-flown terrain referred as height in real time.

ASELSAN Interference Blanker Unit (aselPINE AIBU) is used on military platforms to prevent interference between the numerous onboard RF systems.

aselPINE DCU collects analog, discrete and digital data from various avionic and aircraft systems

aselPINE GIU (Gun Interface Unit) is the interface unit to manage and fire the gun of T-129 ATAK. It provides discrete and power signals required.
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aselPINE SIU collects various analog platform parameters, translates them to digital and presents to use of pilots. Generates analog driving signals that are commanded by mission equipment.

aselPINE WIU (Weapon Interface Unit) is a 2 channel MIL-STD-1760D interface unit. It provides discrete and power signals required to manage and fire two weapon systems simultaneously.

ATRAS is an indigenously developed navigation unit that is designed tooperate both in civil and military aerial platforms.

Main Responsibility of FLCON FCC which is designed for use on GÖKBEY and ATAK-II helicopters, is to provide autopilot functionality to the air vehicle it is mounted. FLCON FCC has all the interfaces which are required to control a rotary wing air vehicle and two powerful CPUs to control these interfaces.

FLCON UKB Flight Control Computer is designed in order to provide multiple reliable interface options, high processing and performance capability for flight sensors, control surfaces, equipments and other avionics sub-systems.

Mission Data Recorder (RECON 100) is an avionic system designed by ASELSAN to compress and record video, audio and mission data.

Crash Survivable Mission Data Recorder (RECON 100C) is an electronic unit designed by ASELSAN to store and protect flight, audio and video data within its protected structure against extreme conditions of an accident.

VYB-4CF is an intelligent microprocessor-based data loading unit. VYB-4CF manages access to mission data or file systems for data storage and retrieval from storage media through Ethernet by using industry standards such as SMB (SAMBA), FTP (File Transfer Protocol) and TFTP (Trivial File Transfer Protocol) file transfer protocols.

SKYMAP is a Digital Moving Map developed by ASELSAN, for T-70 Black Hawk and T-625 Gökbey Utility Helicopters.

TULGAR Helmet Mounted Display (HMD) is a head mounted visor projected display system for fixed wing platforms.

ANS 420-A is an integrated position and attitude determination system with embedded GNSS receiver which is intended for application to air platforms.

ANS 420-L is an integrated position and attitude determination system for land vehicles. ANS 420-L provides linear acceleration, linear and angular velocity, position, attitude to the host vehicle systems continuously.

ANS 510-A is a navigation grade airborne inertial navigation system with embedded GPS/GNSS receiver which is intended for application to air vehicles.

ANS 510-L is an integrated position and attitude determination system for land vehicles. ANS 510-L supplies linear acceleration, linear and angular velocity, position, attitude to the host vehicle systems continuously.

ANS 510-M is a navigation grade naval inertial navigation system with embedded GPS receiver and Log speed interface. It is a small, low-cost, massproducible system that will support a broad spectrum of marine platforms.

ANS 511-A is a navigation grade airborne inertial navigation system with embedded GPS (SAASM) or GNSS receiver which is intended for application to air vehicles.

ANS 530-L is an integrated position and attitude determination system for land vehicles specifically for high-shock artillery gun systems.