IYABOKO · IOSTS Programme · Higher-Tech Research Architecture

Engineer a traceable path from mission evidence to space-system readiness.

IOSTS is IYABOKO’s simulation-first, evidence-gated research and engineering programme for orbital research-spacecraft architectures, connecting digital twins, subsystem telemetry, scientific reference data, verification evidence and accountable Human Authority.

Current Gate Engineering Console Cosmic Satellite Software Research Collaboration
Programme Boundary

Two research tracks. One evidence boundary.

IOSTS-R

Real-World Engineering Research

Conventional engineering models, explicit assumptions, configuration control, subsystem simulation and progressively stronger evidence.

IOSTS-X

Exploratory Future-Physics Research

Falsifiable hypothesis development remains under research HOLD. No engineering promotion without reproducible and independently examinable evidence.

Current boundary: the public implementation remains simulated and non-operational.
R0–R6 Engineering Roadmap

Progress is evidence-gated, not presentation-gated.

R0

Baseline

Mission definition, requirements, assumptions and configuration baseline.

R1 · CURRENT

Integrated Simulation

Power, thermal, avionics, communications, telemetry and FDIR simulation.

R2

Bench Evidence

Low-energy breadboard measurements after scope and safety authorisation.

R3

SIL / MIL / HIL

Software-, model- and hardware-in-the-loop evidence.

R4

Engineering Model

Developmental physical integration after earlier evidence supports progression.

R5

External Review

Independent examination of verification evidence and residual uncertainty.

R6 · NOT CLAIMED

Flight Candidate

Only after qualified evidence, certification and external authority requirements.

AUTHORITY

Human / External

Engineers, institutions, regulators, launch providers and operators retain authority.

SpaceCore · IOSTS-R Digital Twin Mission Laboratory

Disturb the simulated spacecraft. Watch telemetry, evidence and assurance respond.

This public laboratory is a browser-side software simulation. Scientific-reference feeds are kept separate from spacecraft telemetry.

IOSTS-R R1 INTEGRATED SIMULATION SIMULATED TELEMETRY SPACECORE EVIDENCE SENTINEL HUMAN GATE FLIGHT AUTHORITY NONE
IYABOKO SPACECORE · IOSTS-R MISSION DIGITAL TWIN LIVE SIMULATION
MISSION IOSTS-R-MISSION-R1
FRAME: EARTH-CENTRED
ORBIT: LEO RESEARCH
AUTHORITY AI: NONE
FLIGHT: NONE
HUMAN GATE: REQUIRED
Elapsed0000 s
Altitude550.0 km
Velocity7.59 km/s
Battery86.0 %
Thermal28.0 °C
Comms98 %
Public Demonstration Boundary. IOSTS-R telemetry shown here is simulated. External NASA/JPL/CelesTrak information, when available, is a read-only scientific reference and is not spacecraft telemetry. No propulsion, radio, HIL actuator, flight computer or physical spacecraft command route is exposed.
Higher-Tech Architecture

One evidence-centred research stack.

HT-01

Mission Digital Twin

Deterministic spacecraft, orbit and subsystem state simulation.

HT-02

FDIR Runtime

Fault detection, isolation, recovery state and controlled safe-mode logic.

HT-03

Scientific Reference Plane

External ephemeris, catalogues and environment data with explicit provenance.

HT-04

SpaceCore Evidence

Source receipts, timing, transformation state and verification context.

HT-05

C3 / CoreINTEL

Governed computation, modelling, requirements and project intelligence.

HT-06

Sentinel / SACG

Evidence quality, findings, continuity, uncertainty and readiness gates.

HT-07

BOKOMUTO

Future digital-to-physical engineering and prototype preparation pathway.

HT-08

Human / External Authority

Qualified people and institutions retain consequential decisions.

Mission Definition→ Digital Twin→ Scientific Reference→ Evidence Receipt→ Verification→ Sentinel / SACG→ Human Gate
Next Research Software Programme · ICSS

IYABOKO Cosmic Satellite Software

The proposed ICSS layer extends SpaceCore from spacecraft-system research toward evidence-aware exploration of orbital, planetary, stellar and deep-space datasets.

PLANNED SOFTWARE COSMIC DATA EXPLORATION CATALOGUE + EPHEMERIS PROVENANCE AWARE NO SPACECRAFT CONTROL
ICSS-01 Cosmic Map Engine Multi-scale sky, Solar System and galactic scene graph with catalogue-aware object identity and level-of-detail rendering.
ICSS-02 Orbit & Ephemeris Engine JPL state-vector references, public orbital elements, propagation adapters and time-aware coordinate transformations.
ICSS-03 Exoplanet Explorer Search, filter and visualise planetary systems while preserving catalogue provenance.
ICSS-04 Space Environment Layer Near-Earth-object and space-weather reference overlays separated from simulated mission state.
ICSS-05 Observation & Mission Planner Target selection, visibility windows, research scenarios, constraints and exportable observation plans.
ICSS-06 Evidence Graph Every object and derived result records source, time, transformation, uncertainty and verification state.
ICSS-07 C3 / CoreINTEL Intelligence Query planning, anomaly analysis, model comparison and research context without promoting model output into authority.
ICSS-08 Sentinel Research Gate Separates OBSERVED, CATALOGUE, DERIVED, SIMULATED, HYPOTHESIS and UNVERIFIED information.
ICSS boundary. ICSS should begin as research and exploration software. It is not an operational cosmic satellite, autonomous flight system or deep-space mission until corresponding physical evidence, qualification and external authority exist.
Research Progression

IOSTS-R provides the spacecraft research layer. ICSS becomes the cosmic exploration software layer.

Both can connect through SpaceCore, C3, CoreINTEL, Sentinel, SACG, BOKOMUTO and Core OS while maintaining explicit evidence and authority boundaries.

Space & Aerospace Research Collaboration Validation