SPACEPULSE™
Modern satellite mega-constellations and deep space missions operate far beyond the loop of ground station teleoperation. While autonomous AI planners excel at macro logistics and swarm tasking, stochastic neural models cannot be given direct thruster or flight-control authority.
SpacePulse solves the aerospace autonomy bottleneck. Operating as a deterministic, flight-grade physical governor in bare-metal #![no_std] Rust, SpacePulse sits strictly between autonomous cognitive software and flight actuators. It mathematically verifies closed-form orbital invariants, enforces approach cones, protects propellant budgets, and prevents unphysical maneuvers in real time.
Why AI Planners Cannot Have Direct Actuator Authority
Autonomous mega-constellations cannot rely on human ground-station intervention. But giving neural models unvetted control of physical thrusters introduces catastrophic mission risk.
AI Hallucinations in Flight
Autonomous LLMs and cognitive agents can miscalculate orbital perturbations, request unphysical slew paths through blinding solar keep-out zones, or exhaust fuel reserves in singular maneuvers. A single unvetted burn can destroy an entire spaceflight asset.
The SpacePulse Physical Governor
SpacePulse forms an unyielding boundary. Every high-level command is intercepted and mathematically validated against instantaneous power budgets, structural thermal constraints, propellant mass reserves, and relative collision drift envelopes.
Cybernetic Fallback Co-Pilot
When an unsafe maneuver is vetoed, SpacePulse does not simply freeze. Its embedded fallback co-pilot automatically synthesizes a certified, physically optimal recovery maneuver—ensuring the spacecraft remains operational, stable, and power-positive.
Integrated Flight Capabilities
From deterministic 6-DOF attitude kinematics to radiation fault-tolerance across high-radiation orbital passages.
1. Deterministic 6-DOF Attitude Kinematics
Full quaternion attitude kinematics avoiding gimbal lock entirely. Provides exact 6-DOF docking corridor monitoring combining approach cones, angular velocity limits, and reaction wheel torque limits.
2. 4-Rate Cyclic Executive Scheduler
Static rate-monotonic executive executing 100 Hz rate-gyro loops, 10 Hz attitude determination, 1 Hz orbital ephemeris propagation, and 0.1 Hz telemetry and housekeeping broadcasts.
3. Radiation Hardening & TMR Scrubbing
Bitwise 2-out-of-3 Triple Modular Redundancy (TMR) and SEC-DED Hamming error detection. Memory scrubbing rates dynamically scale up to 1000 Hz during orbital passage through high-radiation environments.
4. Autonomous Collision Avoidance
Automated Time to Closest Approach (TCA) and probability of collision solvers that compute fuel-optimal evasive burns against space debris without requiring ground station uplink.
5. Rendezvous & Swarm Station-Keeping
Relative orbital element tracking and closed-form relative motion dynamics for multi-satellite constellation station-keeping and safe passive drift during proximity operations.
6. CCSDS Telecom & Payload Telemetry
Fully compliant with international CCSDS Space Packet Protocols and frame synchronization. Includes deterministic payload telemetry pipelines for high-throughput scientific instrumentation.
Tested Across Flight-Grade Silicon
Engineered in strict #![no_std] Rust with zero dynamic memory allocation on the critical flight path.
| TARGET SILICON | COMPILATION TARGET | FLIGHT PLATFORM | MISSION ROLE |
|---|---|---|---|
| SPARC V8 (LEON3 / LEON4) | sparc-unknown-none-elf | Cobham Gaisler GR712RC / GR740 | Deep-Space Probes, Civil Science Payloads, Class A Onboard Computers |
| ARM Cortex-R4 / R5 / R7 | armv7r-none-eabi | TI TMS570LC4357 / Xilinx Zynq UltraScale+ | Real-Time GNC Actuator Control Nodes, High-Rate Gyro Loops |
| ARM Cortex-M4 / M7 | thumbv7em-none-eabihf | Microchip SAMV71Q21RT (Rad-Tolerant) | SmallSat & CubeSat Swarm Autonomous Flight Computers |
| RISC-V (RV32 / 64IMAC) | riscv32imac-unknown-none-elf | NOEL-V / Microchip PolarFire SoC | Next-Gen Open Radiation-Hardened Aerospace Systems |
Zero-Copy C-ABI & NASA cFS Bridge
Directly embeddable into NASA Core Flight System (cFS), RTEMS, or commercial flight software architectures (include/spacepulse.h).
/* ========================================================================= * SPACEPULSE FLIGHT SOFTWARE EXECUTIVE — NASA cFS TASK EMBEDDING * Target: Spaceflight Avionics Host (LEON3 / Cortex-R5) * ========================================================================= */ #include "spacepulse.h" #include <stdio.h> void SpacePulse_cFS_App_Task(void) { SpacePulseAgenticExecutive* pExecutive = NULL; // 1. Allocate and initialize SpacePulse executive SpacePulseStatus status = spacepulse_agent_create(&pExecutive); if (status != SpacePulseStatus_Success) return; // 2. Define satellite orbit & health state KeplerianStateFFI orbit = { .semi_major_axis_km = 6878.137, .eccentricity = 0.001, .inclination_rad = 0.90, }; SpacecraftHealthState health = { .battery_soc_pct = 98.0f, .bus_voltage_v = 28.0f, }; ExecutiveCycleOutput output; // 3. Step 100 Hz deterministic flight loop (< 100 µs execution) status = spacepulse_agent_step(pExecutive, &orbit, NULL, 0, &health, 0.01, &output); if (status == SpacePulseStatus_Success) { printf("[SPACEPULSE OK] Governor Verified • Actuators Commanded\n"); } spacepulse_agent_destroy(pExecutive); }
Acquire or License the SpacePulse™ FSW
SpacePulse is a completed, flight-ready software asset engineered by Saiwalo Labs. It is packaged with hardened `#![no_std]` Rust crates, multi-rate cyclic executives, NASA cFS headers, and automated hardware-in-the-loop (HIL) test suites.
Available for outright intellectual property acquisition, exclusive commercial constellation licensing, or strategic aerospace integration by satellite primes, defense commands, and deep-space mission operators.