01
Frame a requirement
Start with an ML-D mission, a bounded configuration, and a claim the accepted runtime can actually test.
Mission objective · success criterion · declared limitation
Open the reference ML-D missionUniversity engineering · ML-D Mission Systems
Move from an undergraduate mission requirement into the accepted Mission Control workspace. Inspect model identity, units, provenance, fidelity and lineage; compare deterministic replays; export evidence; and state exactly what the software does not validate.
Academic depth
ML-D · Mission Systems
Mission catalogue
13 pilot missions
Engineering surface
Mission Control
Truth boundary
SIMULATED · 0 measured
The academic demand changes; model ownership and physical truth do not.
Use the accepted Core through a versioned, curated software interface without creating a university physics fork.
A coherent route from requirement framing to evidence review, using accepted lessons and Mission Control.
01
Start with an ML-D mission, a bounded configuration, and a claim the accepted runtime can actually test.
Mission objective · success criterion · declared limitation
Open the reference ML-D mission02
Use the university 3U teaching definition and inspect the selected model bindings before interpreting results.
Spacecraft definition · model/version identity · configuration hashes
Inspect advanced identity03
Execute one deterministic software-only practice run, then inspect units, channel roles, source models, and freshness.
Immutable local replay · simulated and derived channels · zero measured channels
Enter engineer Mission Control04
Use the existing same-seed comparison to study how the school 1U and university 3U teaching definitions change the run.
Shared seed · synchronized replay cursor · baseline/variant deltas
Open synchronized comparison05
Separate availability, provenance, fidelity, calibration, validation, and parameter source instead of collapsing them into one quality label.
Independent fidelity axes · lineage · limitations · Evidence V2 export
Review fidelity and lineage06
Faculty can map MissionLab outcomes and evidence into their own approved CLOs without transferring accreditation authority to CubeSTEM.
Illustrative CLO label · MLO trace · mission evidence · assessment method
Review mapping examplesThey share model truth while exposing different levels of engineering detail.
Guided disclosure
Boundaries
Engineer and advanced disclosure
Boundaries
Mission Control already owns these presentation capabilities; the university journey points into it rather than creating a parallel dashboard.
| Layer | What engineers can inspect |
|---|---|
| Configuration | University 3U teaching definition and bounded scenario selection |
| Model identity | Component/model IDs, versions, provider context, and hashes |
| Channels | Units, roles, source fields, freshness, and explicit availability |
| Provenance | Simulated, derived, reference, estimated, and measured remain distinct |
| Fidelity | Representation, fidelity, calibration, validation, and parameter source stay independent |
| Lineage | Definition, execution, compile, run, frame, and evidence identities where provided |
| Evidence | Same-seed compare, immutable local replay, limitations, JSON and Markdown exports |
| V&V boundary | Software evidence supports bounded conclusions, not flight qualification |
Non-official demonstration content showing how faculty could frame existing missions. These examples are not institution-reviewed mappings or endorsements.
Space systems · controls · electrical power
A student team traces a declared attitude change into modeled solar-energy evidence, checks reproducibility, and writes a bounded V&V conclusion.
Mission operations · communications · systems engineering
A student team distinguishes modeled visibility from reception and decode, then produces a requirements-based contact-plan evidence review.
Every item remains a PILOT_LESSON pending educator review and classroom evidence. ML-D adds engineering disclosure and V&V demand, not new physics.
Choose an orientation strategy by comparing how pointing changes modeled solar-energy collection.
Find a modeled visibility window and make a contact plan without claiming signal reception or data delivery.
Compare two spacecraft profiles through the same modeled eclipse and recommend the more resilient energy strategy.
Separate simulated truth from estimated state while comparing perfect and realistic instruments.
Inspect a bounded deployment sequence and decide which step prevents a safe first-contact attempt.
Compare two bounded control responses and recommend the one that best balances pointing accuracy and actuator demand.
Compare modeled detumble responses and select the damping strategy that reaches a stable state most effectively.
Compare two spacecraft under the same modeled workload and recommend the one that manages temperature and energy more effectively.
Choose a camera profile by balancing modeled image detail against storage and downlink delivery.
Evaluate two declared configurations against every modeled mission budget and choose which can proceed.
Trace the modeled failure sequence and recommend one policy change that addresses the decisive cause.
Use modeled fault evidence to write one testable condition-and-action policy rule.
Test whether a claim based on a short observation remains supportable after a longer run of the same model and seed.