PRODUCT · SPC-AP FAMILY
One flight control computer. Four ways to deploy it.
A reconfigurable FPGA autopilot for drones, UAVs and UGVs. New sensors, protocols or security modules arrive in the field as firmware, not as a new board.
SPC-AP-DEV
SPC-AP-CORE
SPC-AP-DEF
SPC-AP-SIM
SPC-AP-DEV
Developer module
Open stack for integrators and research teams.
SPC-AP-CORE
Commercial flight computer
The production module on its carrier board.
SPC-AP-DEF
Defence-grade variant
Rugged housing, sealed circular connectors.
SPC-AP-SIM
Hardware-in-the-loop unit
Test flight software on real hardware.
INSIDE THE MODULE
Four layers, one sealed module.
SPC-AP · ASSEMBLY SEQUENCE · PRODUCT RENDERSTEP 01 / 06Carrier boardThe only part that changes per airframe. Pixhawk-compatible I/O and antenna ports.
STEP 02 / 06Triple-redundant IMU coreThree inertial sensors on a board suspended by vibration dampers.
STEP 03 / 06FPGA flight computerThe reconfigurable SoC that runs control, navigation and security in parallel hardware.
STEP 04 / 06Sealed aluminium housingCNC-machined, with a conducted thermal path and the status light.
STEP 05 / 06Assembled and readyOne module. One integration. Ready to fly.
STEP 06 / 06Serviced from the topTop-down disassembly for inspection, upgrades and repair.
CARRIER BOARD
Your airframe, your connectors.
The carrier board holds every external interface. A new platform gets a new carrier, while the flight core and its qualification stay the same.
01Actuator and serial I/O
02CAN-FD and telemetry
03Sensor expansion
04Dual GNSS antennas
05Sealed flight core
06Status light
INTERFACE GROUPS · ILLUSTRATIVEKEY SPECIFICATIONS
What is in the module.
Detailed performance data is shared with qualified customers under NDA, subject to export regulations.
Form factor40 × 40 mm core, Pixhawk-compatible connector layout
ProcessingReconfigurable FPGA system-on-chip, parallel hardware control architecture
Control loopAbove 1 kHz with guaranteed timing
SensorsTriple-redundant IMU, dual-redundant GNSS, barometer and magnetometer
NavigationGNSS-independent navigation with FPGA-accelerated LiDAR SLAM and visual-inertial odometry
EW resilienceGNSS anti-spoofing monitoring, jamming detection, CRPA antenna interface
SecurityHardware AES-256 encrypted datalink, Trusted I/O Processor
EnvironmentDesigned to MIL-STD-810G environmental conditions
PlatformsFixed-wing, multirotor and VTOL UAVs, unmanned ground vehicles
AVAILABILITYEvaluation program in 2027. First deliveries from Q2 2028.
Reserve evaluation units