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North Atlantic SIU34-FCCVARM-01 Flight Control Computers

4x 3U OpenVPX MOSA Flight Control Computer

8 x ARINC-429 Tx/Rx & 12 Programmable Discrete IO (CM2)
16 x ±100 VDC A/D Channels (ADF)
8 x Programmable RS-232/422/485 Serial Channels (SC3)
2 x AC Excitation References (AC2)
4 x LVDT Measurement Channels (LD2)
4 x ±40 VDC 100 mA Digital to Analog Channels (DA3)
28 VDC Input PSU per VITA 62 (VPX68) with at least 50 ms holdup
MIL-STD-810G, MIL-STD-461F and DO-160 environmental and EMI/EMC qualifications.

SKU: SIU34-FCCVARM-01 Category: Uncategorized

Flight Control Computers (FCC): Flight Control Computers (FCC) systems are used to support several platform flight control systems including fixed-wing aircraft, rotary aircraft, eVTOL and rocket systems. These Modular Open Systems Approach (MOSA) systems feature different analog and digital input and a wide range of communication types including MIL-STD-1533, ARINC-429, RS-232/422/485 and CANBus A/B 2.0/CAN-FD/ARINC-825. NAI’s rugged FCC systems offer a DO-178C & DO-254 Certifiable solution and are ruggedized to withstand -40° C to +71° C and qualified to MIL-STD-1275D & MIL-STD-704A with 50 ms holdup (power supply); MIL-STD-461F & MIL-STD-810G.

SIU34-FCCVARM-01 is a Modular Open Systems Approach (MOSA) DO-178C & DO-254 Certifiable Flight Control Computer (FCC) with low power high performance OpenVPX Xilinx UltraScale+ SBC with Quad Core ARM Cortex -A53, 8 GB DDR4 SDRAM, 32 GB SATA Flash, 2 x 10/100/1000Base-T Ethernet, USB 3.0, FIPS-140-3 Level 3 Cyber Security, and Single Event Upset support.

North Atlantic SIU34-FCCVARM-01 Flight Control Computers

Key Features

Configured to support dual or tri-redundancy using Serial CCDL or ARINC-429/575 Interfaces. Options for TSN, TTE, AFDX or ARINC664p7 redundancy are also available.

2 x MIL-STD-1553 & 8 x ARINC-429 Tx/Rx (CM5)
8 x Programmable RS-232/422/485 Serial Channels (SC3)
8 x CANBus A/B 2.0/CAN-FD/ARINC-825 (CB8)
4 x AC Excitation References (2 x AC2)
4 x LVDT Measurement Channels (LD2)
4 x Synchro/Resolver Measurement Channels (SD2)
8 x ±40 VDC 100 mA Digital to Analog Channels (DA3)
24 x Enhanced Programmable Discrete I/O Channels (DT4)
16 x Enhanced Differential Discrete I/O Channels (DF1)
16 x ±100 VDC A/D Channels (ADF)
28 VDC Input PSU per VITA 62 (VPX68) with at least 50 ms holdup.
MIL-STD-810G, MIL-STD-461F and DO-160 environmental and EMI/EMC qualifications.

Key Benefits

The SIU34-FCCVARM-01 is ideally suited to support several platform flight control systems including fixed-wing aircraft, rotary aircraft, eVTOL and rocket systems. The SIU34-FCCVARM-01 takes advantage of NAI’s COSA Architecture: a flexible, adaptable, configurable, modular and expandable solution that offers an almost infinite number of configurations while eliminating hardware and software NRE redesign. Certifiable RTOS support includes DDC-I Deos 653 and Wind River VxWorks HVP

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For more than 50 years, Integrys has been the industry leader in selecting and evaluating rugged and embedded computers, imaging and video technology and engineering solutions.

Specifications

Need more or less configurations than the SIU34-FCCVARM-01? Choose from NAI’s standard COTS configurable systems that you can populate with pre-integrated boards, smart function modules, power supplies and software libraries of your choice.

Model	Dimensions w/ Connectors (w x h x d)	Weight / lbs. (Fully populated)	Function Module Slots	Board Slots	Board Formats
NIU1A	6.8” x 1.5” x 2.5”	< 1.2	1	N/A	Integrated System
NIU2A	7.0” x 3.0” x 2.5”	< 2.75	2	N/A	Integrated System
NIU3A	7.2″ x 5.65″ x 3.25″	< 5.4	3	N/A	Integrated System
NIU3E	7.2″ x 6.6″ x 3.0″	< 6	1	N/A	Integrated System
SIU31	4.71” x 2.35” x 8.71”	< 5	3	1	cPCI
SIU32 Preliminary	9.4” x 5.7” x 3.9”	< 11	6	2	OpenVPX
SIU33	4.71” x 4.78” x 8.71”	< 10	9	3	cPCI
SIU33V	4.71” x 4.78” x 8.71”	< 10	9	3	OpenVPX
SIU34	9.4” x 5.7” x 5.9”	< 16	12	4	OpenVPX
SIU35	7.13” x 4.76” x 8.71”	< 15	15	5	cPCI, OpenVPX
SIU36	7.13“ x 4.71“ x 8.91“	< 23	18	6	OpenVPX