A formal certification platform for embedded control algorithms and critical AI systems. GNC controllers, embedded AI models, FPGAs, DSPs, microcontrollers — any discrete linear system certified with formal guarantees within the certified domain and documented assumptions. Not simulation. Not statistics. Mathematically traceable certification in under one second.
No simulation. No weeks of manual analysis. Submit your system matrix and receive a formally guaranteed PDF certificate in under one second. Your data never persists — encrypted in transit, processed in memory, deleted after certification.
Upload the state-transition matrix of your algorithm — GNC controller, Kalman filter, SSM model, PD attitude control. Just numbers. No mission data, no chip architecture, no IP exposed.
Data encrypted with TLS in transit. Processed in server memory only. Automatically deleted after certification. Zero data retention. Your matrix is mathematically anonymous.
STARS verifies convergence across all subsystems using the unified contraction parameter. The result is a formal mathematical proof — not a statistical estimate.
A PDF with unique SHA-256 ID, UTC timestamp, contraction parameter, ISS error bounds, convergence steps, CERTIFIED / REJECTED verdict. Compatible with ECSS, IEC 61508, ISO 26262, DO-178C.
Each module is backed by formally verified mathematical discoveries, cross-validated on real mission data from ESA, NASA, and NOAA across 23 agencies and 74 satellites.
STARS certifies the embedded control algorithm — not the silicon. If a chip implements a discrete linear controller, Kalman filter, SSM model, or PD attitude control, STARS provides algebraic certification in under one second.
Quad-core rad-hard SoC on ESA EPPL. Used in ESA JUICE, Proba-3. GNC controllers certifiable with D#15 and D#7.
Dual-core rad-hard LEON3FT on ESA EPPL. Used in Sentinel-3, OPS-SAT, CHEOPS. Standard processor for ESA small/medium missions.
LEON3FT with real-time accelerators. Used in ESA CubeSats and small missions. D#7 certifies PD attitude control algorithms running on GR716B.
8-core NOEL-V RISC-V + LEON4FT + eFPGA. First rad-hard AI chip for space. D#16 certifies SSM models for on-orbit AI inference.
150K LE rad-hard Flash FPGA, SEU-immune. Implements GNC controllers at 100Hz. D#15 and D#7 certify all discrete control algorithms.
Antifuse rad-hard FPGA, 300 krad. Flight heritage on MRO, Cassini. GNC algorithms with no formal algebraic certification today — STARS fills that gap.
ARM Cortex-M7 rad-hard, 150 krad. SpaceWire + MIL-STD-1553 + CAN-FD. D#7 certifies attitude PD controllers on SAMRH707.
NASA next-gen SoC, 100x RAD750 performance. Designed for autonomous spacecraft decisions. Testing at Goddard 2026. Prime candidate for STARS certification.
Most proven space processor — Mars rovers, New Horizons, James Webb, Juno. Thousands of active missions with GNC algorithms that have no formal certification today.
Versal AI Core space-grade. ARM + AI Engine + FPGA, 4 TOPS. D#16 certifies SSM models on AI Engine for Earth observation and autonomous navigation.
Kintex UltraScale space-qualified, 726K logic cells. Used in Airbus, Thales, and NewSpace satellites. Implements control algorithms without formal algebraic certification.
ARM Cortex-M4 rad-hard, 300 krad. Used in commercial CubeSats and small LEO satellites. D#7 provides certified PD gains for attitude control.
ARM Cortex-M4, QML certified by DLA — highest space-grade standard. QPL part 5962-R24203. D#7 certifies attitude control algorithms on VA41630.
Rad-hard SBC based on NASA H-Core. Used for command and data handling in micro/nanosatellites. D#6 certifies orbital estimators running on Proton200k.
Triple-core rad-hard DSP for LEO and GEO satellites. D#15 certifies discrete control loops. D#6 certifies orbital navigation algorithms on Proton400k.
STARS certifies the embedded control algorithm — not the physical silicon. Hardware failures (radiation SEUs, thermal degradation, manufacturing defects) remain the domain of FMEA, radiation testing, and hardware qualification. STARS provides the formal algebraic certification layer that has never existed before.
The algebraic guarantee is domain-agnostic. The same formal proof that certifies a satellite FPGA certifies an industrial robot controller, an automotive ECU, or a medical device SSM model.
FPGAs, processors, AI chips in LEO/GEO/deep space. ECSS-E-ST-60-10C compatible. 2–6 weeks reduced to seconds. Validated on 74 real satellites across 23 agencies.
Flight control chips under EU AI Act high-risk classification. D#7 certifies PD attitude control on any UAV flight controller. EASA compliance for commercial drone operations.
Closed-loop controllers on industrial robot MCUs and FPGAs. D#15 certifies any discrete control loop under IEC 61508 SIL 2/3. Certification in under 1 second vs weeks of manual Lyapunov analysis.
Embedded SSM models on medical chips for continuous monitoring. D#16 provides the formal convergence guarantee required for high-risk AI under MDR and FDA IEC 62304.
Independent validation campaign using real public parameters from ESA eoPortal, University of Colorado Boulder, Cal Poly CubeSat Lab, NASA SmallSat SOA, and manufacturer datasheets. All 50 certifications passed across 15 chip families. Algebraic consistency: 100%.
| Chip | Fabricante | Algoritmo | Módulo | Alpha | Veredicto |
|---|---|---|---|---|---|
| Gaisler GR740 | Cobham Gaisler / ESA | Attitude PD Control | D#7 | 0.4524 | ✦ CERT |
| SSM / Mamba (dim=3) | D#16 | 0.3759 | ✦ CERT | ||
| GNC System Matrix | D#15 | 0.4848 | ✦ CERT | ||
| GPS Eclipse Navigation | D#6 | 0.1378 | ✦ CERT | ||
| Gaisler GR712RC | Cobham Gaisler / ESA | Attitude PD Control | D#7 | 0.4224 | ✦ CERT |
| SSM / Mamba (dim=3) | D#16 | 0.3439 | ✦ CERT | ||
| GNC System Matrix | D#15 | 0.4565 | ✦ CERT | ||
| GPS Eclipse Navigation | D#6 | 0.1378 | ✦ CERT | ||
| Gaisler GR716B | Cobham Gaisler | Attitude PD Control | D#7 | 0.4816 | ✦ CERT |
| SSM / Mamba (dim=3) | D#16 | 0.4071 | ✦ CERT | ||
| GNC System Matrix | D#15 | 0.5122 | ✦ CERT | ||
| Gaisler GR801 GRAIN | Cobham Gaisler | Attitude PD Control | D#7 | 0.5100 | ✦ CERT |
| SSM / Mamba (dim=16) | D#16 | 0.3111 | ✦ CERT | ||
| GNC System Matrix | D#15 | 0.5390 | ✦ CERT | ||
| Microchip RTG4 | Microchip Technology | Attitude PD Control | D#7 | 0.5376 | ✦ CERT |
| SSM / Mamba (dim=3) | D#16 | 0.3600 | ✦ CERT | ||
| GNC System Matrix | D#15 | 0.5649 | ✦ CERT | ||
| Microchip RTAX2000S | Microchip Technology | Attitude PD Control | D#7 | 0.4375 | ✦ CERT |
| SSM / Mamba (dim=3) | D#16 | 0.3600 | ✦ CERT | ||
| GNC System Matrix | D#15 | 0.4707 | ✦ CERT | ||
| Microchip SAMRH707 | Microchip Technology | Attitude PD Control | D#7 | 0.4671 | ✦ CERT |
| SSM / Mamba (dim=3) | D#16 | 0.3916 | ✦ CERT | ||
| GNC System Matrix | D#15 | 0.4986 | ✦ CERT | ||
| Microchip HPSC (NASA) | Microchip / NASA JPL | Attitude PD Control | D#7 | 0.4816 | ✦ CERT |
| SSM / Mamba (dim=12) | D#16 | 0.3276 | ✦ CERT | ||
| GNC System Matrix | D#15 | 0.5122 | ✦ CERT | ||
| GPS Eclipse Navigation | D#6 | 0.1378 | ✦ CERT | ||
| BAE Systems RAD750 | BAE Systems | Attitude PD Control | D#7 | 0.4375 | ✦ CERT |
| SSM / Mamba (dim=3) | D#16 | 0.3600 | ✦ CERT | ||
| GNC System Matrix | D#15 | 0.4707 | ✦ CERT | ||
| AMD Versal XQRVE2302 | AMD / Xilinx | Attitude PD Control | D#7 | 0.4959 | ✦ CERT |
| SSM / Mamba (dim=32) | D#16 | 0.2604 | ✦ CERT | ||
| GNC System Matrix | D#15 | 0.5257 | ✦ CERT | ||
| AMD Kintex XQRKU060 | AMD / Xilinx | Attitude PD Control | D#7 | 0.5239 | ✦ CERT |
| SSM / Mamba (dim=3) | D#16 | 0.3916 | ✦ CERT | ||
| GNC System Matrix | D#15 | 0.5520 | ✦ CERT | ||
| VORAGO VA10820 | VORAGO Technologies | Attitude PD Control | D#7 | 0.4671 | ✦ CERT |
| SSM / Mamba (dim=3) | D#16 | 0.4224 | ✦ CERT | ||
| GNC System Matrix | D#15 | 0.4986 | ✦ CERT | ||
| VORAGO VA41630 QML | VORAGO Technologies | Attitude PD Control | D#7 | 0.4959 | ✦ CERT |
| SSM / Mamba (dim=3) | D#16 | 0.4071 | ✦ CERT | ||
| GNC System Matrix | D#15 | 0.5257 | ✦ CERT | ||
| Space Micro Proton200k | Space Micro | Attitude PD Control | D#7 | 0.5100 | ✦ CERT |
| SSM / Mamba (dim=3) | D#16 | 0.4375 | ✦ CERT | ||
| GNC System Matrix | D#15 | 0.5390 | ✦ CERT | ||
| GPS Eclipse Navigation | D#6 | 0.1378 | ✦ CERT | ||
| Space Micro Proton400k | Space Micro | Attitude PD Control | D#7 | 0.4959 | ✦ CERT |
| SSM / Mamba (dim=3) | D#16 | 0.4224 | ✦ CERT | ||
| GNC System Matrix | D#15 | 0.5257 | ✦ CERT | ||
| GPS Eclipse Navigation | D#6 | 0.1378 | ✦ CERT |
All chip parameters come from public sources: ESA eoPortal, peer-reviewed papers, university theses (University of Colorado Boulder, Cal Poly), NASA technical reports, and manufacturer datasheets. These are validation simulations — not certifications of actual deployed systems.
3 free certifications. No credit card. No time limit. Full pipeline — GNC, SSM, NAV, ATT.