AMMS
Aircraft and Mission Management System
The AMMS is a powerful computing system designed to provide processing features to rotary wing aircraft, including Navigation & Flight Management, Cockpit Display Management, and Aircraft Plants Management.
The System is composed of:
- Two AMMCs Units (the Computer Core)
- Two Data Transfer Units
- A Control Panel
The AMMS provides the capabilities to acquire, process, and manage information and aircraft plant data from EFIS/EICAS, relevant CNI equipment, and AFCS, in a reliable, high performance environment. It is based upon a core consisting of two identical computers (AMMC, Aircraft and Mission Management Computers), synchronised and concurrently performing the same operations in a master/hotstandby architecture, which allows, in case of failure of the Master, a totally automatic reconfiguration for all system functionalities, therefore resulting in a high mission availability.

- Key Features
- Key Benefits
- Product Datasheet
- Redundant LRI configuration
- PowerPC G4 MCS-E 500Mhz processor
- Easy addition of additional processor module and I/O
- I/O configuration for different aircraft
- COTS RTOS based on I-178B by Green Hills
- Dedicated equipment software and ADA
development environment for application - Digital maps: symbol generation & vectorial layers
- Synthetic voice generator
- Redundant MIL-STD 1553B I/F operates as BC/BM/RT
- High communication throughput
- Ethernet 10/100 baseT
- MIL-STD-1553b
- ARINC 429
- ARINC 739
- RS485 HDLC
- AFDX Copper/Optical I/F compliant with ARINC664
- High data storage capability (up to 8GB)
- Civil specification compliance
- RTCA/DO-160D
- RTCA/DO-254
- RTCA/DO178B
Flight Management System (FMS)
- Area Navigation Management
- Tactical Patterns Management
- Navigation Database Management
- Navigation Display data management
- Helicopter and Navigation Performance computation
- Horizontal and Vertical Steering commands generation for AFCS.
Data Control and Equipment Management/Preset
- Mission Equipment
- Communication/Identification Equipment
- Navigation Sensors.
Aircraft Systems Interfacing, Data Acquisition, Status monitoring and Alert generation
- Engines - Rotors and Transmission - Hydraulics - Electrical - Fuel.
Helicopter plants Health and Usage Monitoring and
Maintenance (HUMS)
- Vibration signal acquisition and processing for
Transmission Monitoring - Engines Health and Usage Monitoring
- Structural Usage Monitoring.
Display Management for EICAS and Navigation
information
Digital Map and Symbol Generation for tactical
symbol capability
- Helicopter Data Upload/Download
- Navigation and COMMS Data
- Map and Mission Data
- HUMS Data
- Maintenance Data