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CubeSTEM MissionLab Twin · M1.1

From Deployment to First Contact

Student prediction, controlled experiment and engineering evidence sheet. The complete activity works without physical hardware.

Open mission
1

Mission question

How can the CubeSat reduce its tumble, recover power, point toward Earth and deliver its first packet without creating excessive overshoot, energy use or actuator stress?

2

Prediction before running

3

Controlled experiment plan

4

Telemetry evidence

MetricBaseline runChanged runBetter / worse / same
Mission score   
Maximum overshoot   
Settling time   
Final battery   
Peak link quality   
Packet attempts   
Anomaly response   
5

Explain the spacecraft behavior

6

Telemetry provenance

Classify at least five channels from your run. M1 software-only mode contains no measured hardware channels.

ChannelProvenanceWhy?
   
   
   
   
   
Simulated: Physics or subsystem state produced by a model
Estimated: A sensor-style estimate derived from simulated truth
Commanded: A validated controller or mission command
Reference: A target or desired mission value
Derived: A calculated value such as pointing error or link quality
7

Conclusion and next test

8

Teacher evidence check

Fidelity boundary: M1 uses authoritative F1 one-axis attitude physics plus deterministic teaching-grade mission systems. It is not a continuous three-axis spacecraft simulation, certified pass prediction, flight-qualification tool or hardware authorization.