Aegis-Orbital Single-Bus Autonomous Foundry & Refining Depot (REV31): A Decentralized Asymmetric Multiprocessing Toolchain and RTL Core Netlist for Orbitally Decoupled Processing Swarms
Year: 2026
Type: software
Abstract: Project Description Project Title: Aegis-Orbital Single-Bus Autonomous Foundry & Refining Depot (REV31)Subtitle: A Decentralized Asymmetry Multiprocessing Toolchain and RTL Core Netlist for Orbitally Decoupled Processing SwarmsDesign Authority: Zachary August JacobyRelease Version: Revision 31 Immutable Checksum Manifest BaselineClassification: Standalone Spoke Repository // Independent Open-Science Specification Executive Summary & System Vision Project Aegis-Orbital Phase 2/3 establishes the complete physical layout parameters, cross-plane multi-core software contracts, and hardware description subsystems for a decentralized Co-Orbital Recycling Sanctuary Phased Array Depot Hub. Moving entirely away from high-mass, monolithic space stations vulnerable to catastrophic thermal back-flooding and structural failures, this architecture implements a fluid-decoupled, distributed swarm flight paradigm running natively within a designated Low-Earth Orbit (LEO) graveyard band. The sanctuary depot operates as an uncrewed network of autonomous functional hardware nodes flying in a dynamically managed phased-array orbital formation. The swarm maintains spatial cohesion via non-fluidic electromagnetic stabilization, millimeter-wave RF mesh data links, and multi-source covariance-weighted matrix tracking loops. By isolating high-temperature structural metallurgy, actively tempered hypergolic propellant storage, and sub-nanosecond processing fabrics into physically independent structural vehicles, Phase 2/3 completely eliminates cross-subsystem thermal fatigue, prevents volatile auto-ignition cascades, and provides near-infinite scaling margins for in-situ orbital commodity tokenization. Core Repository & Microarchitectural Architecture The compressed deployment package contains exactly 39 structurally synchronized files forming a zero-deficit architectural freeze [ysD9J5]. The code blocks, build scripts, and physical layouts enforce the following system parameters: Rigid Word-Aligned Telemetry Frame: Enforces an absolute 88-byte packet blueprint across all network injection pipelines (<QQLLHHBB64s2x), combining a 30-byte header with a 64-byte Ed25519 signature payload and 2 trailing tail-padding bytes to perfectly match GCC’s __attribute__((packed, aligned(4))) rounding behavior on 64-bit interconnect crossbars [ysD9J5]. Asymmetric Multiprocessing Isolation: Integrates a bare-metal ARM Cortex-M4 Sentinel core for hard real-time 10-µs periodic interrupt scheduling loops and an ARM Cortex-M7 core managing an asynchronous Zephyr RTOS logistics layer [ysD9J5]. Strict Memory Segment Zoning: Links the immutable administrative governance matrix (law_matrix_stub.c) exclusively to a hardwired segment inside the Cortex-M4 Tightly-Coupled Memory (DTCM) starting at address 0x20004000, while the M7 core safely parses token transaction data asynchronously over a shared volatile address bus window [ysD9J5]. Pipelined Hardware Offloading: Routes high-overhead TLS 1.3 cryptographic handshakes and Proof-of-Authority (PoA) signature validations directly to a space-grade Xilinx Kintex UltraScale+ FPGA fabric, protecting the core processors from localized micro-trace hotspots and long-term electromigration [ysD9J5]. Sub-Nanosecond Asynchronous Emergency Gating: Configures a balanced 500 MHz reference clock tree with unclocked combinational paths that route critical tracking alarms straight to Triple Modular Redundant (TMR) majority voter clear pins, closing safety actions within a strict sub-4.0 nanosecond window [ysD9J5]. Watertight Thermodynamic Isolation: Mandates an absolute Dual-Path Physically Isolated Manifold Constraint within the propellant storage depot, routing fuel-grade anhydrous hydrazine and nitrogen tetroxide oxidizers through entirely distinct, non-intersecting hardware plumbing channels to neutralize toxic auto-ignition risks [ysD9J5]. Automated Verification & Simulation Testbenches The repository includes a comprehensive, multi-phase continuous integration suite built to validate execution transport lags and telemetry structure boundaries under simulated multi-node kinetic conditions [ysD9J5]: lvds_hil_test.py: Simulates high-speed parallel LVDS data injection tracking profiles, utilizing statistical sample collection and a 95% outlier rejection filter to eliminate host operating system context-switching noise and isolate true microarchitectural propagation delay [ysD9J5]. swarm_hil_simulator.py: Validates inter-node mesh network injection lag and enforces real-time software emulation delay boundaries over the 88-byte structure blueprint [ysD9J5]. automated_ci_cd_driver.py: Initializes a local DAG state-trie ledger state machine, executes hardware-layer data-coherency buffer check loops, and verifies fixed-point division safety against the space-native 2.5% asset decay tariff past the 5,500 LEO cycle chronological epoch limit [ysD9J5]. Ecosystem Rights, Evaluation, & Licensing This repository is published as a standalone Spoke Matrix under Ecosystem Standard Operating Procedure (SOP-01)and utilizes a hybrid open-science evaluation framework: Public Evaluation Clearance: All files, blueprints, and simulation suites are made publicly available under an Open Access status to facilitate absolute academic transparency, decentralized peer verification, and multilateral space-safety compliance audits. Permanent Proprietary Lock: Commercial exploitation, corporate monetization, unauthorized integration, or redistribution of derived modifications is strictly prohibited. The repository is locked to a restrictive open-science boundary to defend the long-term capital stability of the orbital platform. Metadata Registry Index Resource Type: Software (includes Verilog/VHDL netlists, Linker Scripts, C-firmware source, and Python testbenches) [ysD9J5] License Mapping: Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International (CC BY-NC-ND 4.0) Keywords: Aerospace Engineering, Satellite Swarm, Asymmetric Multiprocessing, Fixed-Point Math, High-Performance RTL, Space Salvage, Automated Market Maker, Continuous Integration [ysD9J5]
Author: Jacoby, Zachary August
Language: English
Subfield: Electrical and Electronic Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: green
OpenAlex ID: W7220913724