SkyLabs d.o.o.

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21 Products

13 Years Active

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About SkyLabs d.o.o.

SkyLabs is a space-technology oriented company providing miniaturized on-board data handling solutions and an innovative approach to space engineering. SkyLabs is primarily focused on high-tech tailor-made solution development, including fault tolerant hardware and software development, digital signal processing, radiation hardened by design IP core development, fast prototyping, and space/ground segment communication.

SkyLabs is a vibrant team of electrical, mechanical and computing engineers and scientists providing services and technology solutions for the most demanding terrestrial and aerospace applications. By following the latest technology trends it provides innovative solutions with a proactive and creative design approach.

Its NANOsky avionics product family covers on-board computers (NANOobc-2, NANOhpm-obc, NANOhpc-obc with AI/DPU extensions), an ADCS/GNC platform (NANOadcs, co-developed with Indra Deimos), UHF/VHF, S-band and X-band communication subsystems (NANOcomm-2, NANOlink(-S), NANOcast), an electrical power system with integrated battery management (NANOeps, NANOeps-AMPPT), remote terminal units (NANOif-2, picoRTU), the PicoSkyFT fault-tolerant IP core, and the companion skyEGSE ground support equipment and NANOsky CMM SDK software suite. All designs follow a fault-tolerant, radiation-tolerant-by-design philosophy for nano- and micro-satellite missions.

Company Info

Headquarters Zagrebška cesta 104, 2000 Maribor, Slovenia, EU, SVN

Founded 2013 (13 years)

Specializations

manufacturer obc-avionics communications power adcs-navigation software-services test-equipment

Website skylabs.si ↗

LinkedIn linkedin.com/company/skylabs ↗

Email info@skylabs.si

Sales sales@skylabs.si

Photos 3

Products

TRL 6 · Prototype

High performance GNC platform for ADCS with built-in fault-tolerant OBC, GNSS, magnetometer and gyroscope.

1 9

Standard	ISO 19683, IPC Class 3+
TRL	6
MAIT	In-house
Built-in	NANOhpm interface
Interface	Redundant CAN for TM/TC
Integrated on-board sensors	GNSS receiver, magnetometer, gyro
Configurable LCL protected power channels	3.3V, 5V, 12V, or 18V
Sensors and actuators interfaces	5x RS422, 1x CAN, 4x UARTs, I2C, 12x Analog TIA&NTC, 3x Current ctrl. Full-bridge PWMs, 1PPS I/O
Wide input power range	5V - 28V

TRL 5 · Development

100 Mbps X-band satellite transmission subsystem with integrated amplifier and built-in encryption.

1 9

Standard	ISO 19683, IPC Class 3+
TRL	5
MAIT	In-house
Output power	Up to 37 dBm (5 W)
Security (optional)	AES-GCM-256; CCSDS 355.0-B-2 SDLP
Data rates	Up to 100 Mbps @ 50 MHz (OQPSK)
Interfaces	Redundant CAN for TM/TC, dual LVDS, dual ETH
Protocol	CCSDS compliant
Frequency band	8025 MHz to 8500 MHz

TRL 9 · Flight-proven

UHF/VHF full-duplex satellite communication subsystem with highly efficient amplifier.

1 10

Standard	ISO 19683, IPC Class 3+
TRL	9
MAIT	In-house
Output power	Adj. up to 31 dBm (1.3 W)
Input sensitivity	-111 dBm @ 25 kbps GFSK
Data rates	Up to 25 kbps, full duplex
Frequency band	Tx: 400 - 470 MHz, Rx: 130 - 200 MHz
Protocol	CCSDS compliant
TM storage	Up to 24k log entries
Interfaces	Redundant CAN for TM/TC

TRL 9 · Flight-proven

Highly integrated electrical power system with battery management and power control/distribution module.

1 12

Standard	ISO 19683, IPC Class 3+
TRL	9
MAIT	In-house
Battery pack capacity	Up to 172 Wh (multiple units in parallel configuration)
Battery pack life time	> 30000 re-charge cycles @ 20% DoD (80% EOL capacity)
Charge rate	Continuous up to 18 A
Discharge rate	Continuous up to 18 A, peak up to 54 A
Deployment interfaces	5x deployment outputs, 10x deployment TLM inputs
Separation/RBF switches	Two separation switches and RBF
Battery balancer	Active battery balancing per cell string
Interfaces	Redundant CAN for TM/TC
Power channels	23 independent channels (3 redundant)

TRL 9 · Flight-proven

Safest and most accurate solar array energy conversion subsystem using analog maximum power point tracking.

1 9

Standard	ISO 19683, IPC Class 3+
TRL	9
MAIT	In-house
AMPPT channels	8 channels with dedicated AMPPT each
AMPPT efficiency	> 80% (at 25°C)
Number of NTC inputs	10
Solar array (input) parameters	Input voltage range 12.1V to 23.3V; up to 678 mA input current; input power up to 9W per channel
Charge (output) parameters	Output voltage range 7.5V to 11V; output power up to 8W per channel
Interfaces	Redundant CAN bus for TM/TC

TRL 5 · Development

High-performance, power-efficient AI accelerator extension for NANOhpc-obc using dual Hailo-8 accelerators.

2 8

Standard	ISO 19683, IPC Class 3+
TRL	5
MAIT	In-house
AI extension AI Technology	Dual Hailo-8 accelerator
Performance	Up to 52 TOPS
Typical power	Combined 5W consumption
Supported Frameworks	TensorFlow, TensorFlow Lite, Keras, PyTorch & ONNX
Base NANOhpc-obc Main CPU cluster	4x RISC-V 64-bit processors @ max 600 MHz

TRL 5 · Development

High-performance reconfigurable data processing unit extension for NANOhpc-obc, built around AMD Zynq UltraScale+ MPSoC.

2 12

Standard	ISO 19683, IPC Class 3+
TRL	5
MAIT	In-house
DPU extension AI Technology	AMD Zynq UltraScale+ MPSoC ZU7EV
FPGA Fabric	504K system Logic Cells
Codec support	H.264 / H.265
Dedicated FPGA logic memory	32 Gb DDR4
Application Processing Unit	Quad-core Arm Cortex-A53 @ max 1.5 GHz
Real-Time Processing Unit	Dual-core Arm Cortex-R5F @ max 600 MHz
Graphics Processing Unit	Arm Mali-400 MP2 @ max 667 MHz
Processing system memory	32 Gb DDR4
Base NANOhpc-obc Main CPU cluster	4x RISC-V 64-bit processors @ max 600 MHz

TRL 9 · Flight-proven

64-bit high-performance multicore RISC-V on-board computer for AI@Edge and demanding LEO applications.

2 11

Standard	ISO 19683, IPC Class 3+
TRL	9
MAIT	In-house
Main CPU cluster	4x RISC-V 64-bit processors @ max 600 MHz
Supervisor	RISC-V monitoring core @ max 600 MHz
Main memory	4 GB DDR4
Memory Management	MMU with Physical memory protection
Mass storage	92 GB NAND (EDAC protected)
TM storage	256 kB MRAM with SECDED
Interfaces	Redundant CAN, 4x LVDS/RS422/485/UART/16xGPIO, 2x Gigabit ETH
Software	Linux (Yocto) and real-time OS options

TRL 9 · Flight-proven

High-performance MCU-based fault-tolerant on-board computer.

2 9

Standard	ISO 19683, IPC Class 3+
TRL	9
MAIT	In-house
Processor	NOEL-V 32-bit core (RV32IMAFD) with FPU
Memory	256 MB DDR3 (EDAC protected)
Mass storage	2 GB NAND Flash (EDAC protected)
TM storage	1 MB MRAM (EDAC protected)
Interfaces	Redundant CAN for TM/TC, dual LVDS/RS422/485
On-board	Integrated GNSS receiver

TRL 9 · Flight-proven

Intelligent remote terminal unit with unified TM/TC interface for satellite sensors, instruments and payloads.

1 6

Standard	ISO 19683, IPC Class 3+
TRL	9
MAIT	In-house
User interfaces	2x CAN (with CSP bridge), 5x RS422, 24x ADC, 28x GPIO (8 with remapping to SPI, I2C, UART)
Interfaces	Redundant CAN for TM/TC
TM storage	Up to 24k log entries

TRL 9 · Flight-proven

S-band full-duplex communication subsystem with efficient integrated amplifier and optional AES-256 encryption.

1 11

Standard	ISO 19683, IPC Class 3+
TRL	9
MAIT	In-house
Output power	Adj. up to 30 dBm (1 W)
Security (optional)	AES-GCM-256; CCSDS 355.0-B-2 SDLP; CCSDS 355.1-B-1 SDLP-EP
Input sensitivity	-95 dBm @ 4 Mbps OQPSK
Data rates	Up to 4 Mbps, full duplex
Frequency band	Tx: 2.200 - 2.300 GHz, Rx: 2.025 - 2.110 GHz
Protocol	CCSDS compliant
TM storage	Up to 24k log entries
Interfaces	Redundant CAN for TM/TC

TRL 9 · Flight-proven

S-band communication subsystem with an additional highly efficient amplifier and optional AES-256 encryption.

1 11

Standard	ISO 19683, IPC Class 3+
TRL	9
MAIT	In-house
Output power	Adj. up to 37 dBm (5 W)
Security (optional)	AES-GCM-256; CCSDS 355.0-B-2 SDLP; CCSDS 355.1-B-1 SDLP-EP
Input sensitivity	-95 dBm @ 4 Mbps OQPSK
Data rate	Up to 4 Mbps, full duplex
Frequency band	Tx: 2.200 - 2.300 GHz, Rx: 2.025 - 2.110 GHz
Protocol	CCSDS compliant
TM storage	Up to 24k log entries
Interfaces	Redundant CAN for TM/TC

TRL 9 · Flight-proven

S-band full-duplex communication subsystem with a sophisticated dual-port signal splitter/combiner and optional AES-256 encryption.

1 10

Standard	ISO 19683, IPC Class 3+
TRL	9
MAIT	In-house
Output power	Adj. up to 31.5 dBm (1.4 W) per antenna port
Security (optional)	AES-GCM-256; CCSDS 355.0-B-2 SDLP; CCSDS 355.1-B-1 SDLP-EP
Input sensitivity	-86 dBm @ 4 Mbps OQPSK
Data rate	Up to 4 Mbps, full duplex
Frequency band	Tx: 2.200 - 2.300 GHz, Rx: 2.025 - 2.110 GHz
Protocol	CCSDS compliant
TM storage	Up to 24k log entries

TRL 9 · Flight-proven

Fault-tolerant second-generation on-board computer for mission-critical satellite operation.

2 11

Standard	ISO 19683, IPC Class 3+
TRL	9
MAIT	In-house
Processor	PicoSkyFT 8/16-bit core with single precision FPU
Code Memory	4 MB MRAM (EDAC protected)
Data Memory	2 MB (EDAC protected)
Mass storage	2 GB NAND Flash (EDAC protected)
TM storage	4 Mb MRAM (EDAC protected)
Interfaces	Redundant CAN for TM/TC, dual LVDS/RS422/485
On-board	Integrated GNSS receiver
Software	FreeRTOS OS with NANOsky CMM Framework

Software development kit for control, monitoring and management (CMM) of NANOsky platform subsystems.

1 3

Components	Application Library module (Qt/C++, Windows/Linux) + FW module (C-based, RTOS)
Compatible equipment	NANOobc-2, NANOhpm-obc, NANOlink-2, NANOcomm-2, NANOif, NANOeps, NANOamppt, picoRTU system
FW module functions	Bootloader, FDIR, CAN-TS/LVDS-TS stacks, housekeeping TM, memory & OBT management, software scrubber

TRL 7 · Demonstrated

Highly modular remote terminal unit system for LEO small and micro satellite missions.

5 9

Standard	ISO 19683, IPC Class 3+
TRL	7
MAIT	In-house
Bus interface	Redundant CAN (ISO 11898-2), CANopen per ECSS-E-ST-50-15C
Discrete user interfaces	Compliant with ECSS-E-ST-50-14C specifications
Firmware	Universal, qualified, real-time OS based, per SAVOIR-GS-003
Ground software	skyEGSE-GUI for configuration, integration test and real-time monitoring
Modularity	Standalone base unit or stacked add-on units sharing internal power/RTI bus
Fault tolerance	Radiation-tolerant FPGA, PicoSkyFT core, 3-level FDIR hierarchy

Ground station equipment for CCSDS-compliant, full-duplex communication over S-band RF link with NANOlink-2 equipment.

1 4

Type	CCSDS-compliant SDR ground station equipment
Frequency range	S-band
Error correction	Convolutional and Reed-Solomon codes
Compatible with	NANOlink-2, skyEGSE-GUI, NANOsky CMM SDK

Ground station equipment for CCSDS-compliant, full-duplex communication over UHF/VHF RF link with NANOcomm-2 equipment.

1 4

Type	CCSDS-compliant SDR ground station equipment
Frequency range	UHF/VHF
Error correction	Convolutional and Reed-Solomon codes
Compatible with	NANOcomm-2, skyEGSE-GUI, NANOsky CMM SDK

Intuitive desktop application for out-of-the-box operation, monitoring and control of SkyLabs equipment.

2 4

Type	Windows/Linux desktop application
Connectivity	Via skyEGSE-LINK2 dongle or skyEGSE-comm server
Built on	NANOsky CMM SDK Application Library
Functions	Status overview, real-time TM charting & export, telecommand interface, log download, parametrization, FW upgrade, custom TM/TC execution

USB interface dongle for high-speed, low-latency communication over CAN/LVDS/RS422 interfaces.

1 4

Standard	IPC Class 3+
MAIT	In-house
Interfaces	Two CAN buses, two high-speed LVDS (TIA/EIA-644), two RS422 (TIA/EIA-422)
Connectivity	USB Plug-n-Play

Rad-hard-by-design, fault tolerant 8/16-bit embedded processor IP core (PicoSkyFT) for SoC integration.

1 11

Product code	SKY-9001
Architecture	Harvard enhanced RISC pipelined architecture, ~1 MIPS/MHz
Instruction set	PicoSky ISA with 140 instructions, high code density
Operating modes	Supervisor, User, Debug, Sleep, Reset
Radiation hardening	Radiation hardened by design; all memories EDAC protected (Multiple SEC-DED)
Register protection	Parity protected supervisor and user register files with diagnostic bypass
Traps controller	FDIR policy fully user-definable per fault cause
Program memory models	Compact (8 kB), Small (64 kB), Medium (128 kB), Large (8 MB)
Data memory models	Normal (64 kB) or Extended (16 MB)
Interrupt controller	Configurable, customisable number of prioritised interrupt vectors
Debug facilities	Debug Support Unit (DSU), trace buffer, PicoSkyLINK programmer/debugger interface

Documents

📄 NANOsky Product Catalog

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SkyLabs d.o.o.

About SkyLabs d.o.o.

Photos 3

Products

NANOadcs

NANOadcs

Description

Specifications

NANOcast

NANOcast

Description

Specifications

NANOcomm-2

NANOcomm-2

Description

Specifications

NANOeps

NANOeps

Description

Specifications

NANOeps-AMPPT

NANOeps-AMPPT

Description

Specifications

NANOhpc-AI

NANOhpc-AI

Description

Specifications

NANOhpc-DPU

NANOhpc-DPU

Description

Specifications

NANOhpc-obc

NANOhpc-obc

Description

Specifications

NANOhpm-obc

NANOhpm-obc

Description

Specifications

NANOif-2

NANOif-2

Description

Specifications

NANOlink(-S)-base

NANOlink(-S)-base

Description

Specifications

NANOlink(-S)-boost

NANOlink(-S)-boost

Description

Specifications

NANOlink(-S)-boost-dp

NANOlink(-S)-boost-dp

Description

Specifications

NANOobc-2

NANOobc-2

Description

Specifications

NANOsky CMM SDK

NANOsky CMM SDK

Description

Specifications

picoRTU system

picoRTU system

Description

Specifications

skyEGSE-comm (S-band)

skyEGSE-comm (S-band)

Description

Specifications

skyEGSE-comm (UHF/VHF)

skyEGSE-comm (UHF/VHF)

Description

Specifications

skyEGSE-GUI

skyEGSE-GUI

Description

Specifications