BLACK WIDOWResearch Program
#07Simulation OnlyDIGITAL EVIDENCE ONLY

FlyScout

Hybrid Air/Ground Reconnaissance Micro-Drone

Research Question

Can a 300-400g platform execute aerial-terrestrial transitions with adequate proximity sensing?

Digital Model

Type

Discrete State-Machine

Version

v1.0.0

Plugin

c12_flyscout

Core Variables

3 states (flight, hover, ground), transition events, altitude, descent rate, timing

Main Assumptions

Discrete state transitions; no continuous dynamics; no contact forces; no sensor model; no control loop

Model Boundary

State-machine only; no physics; no aerodynamics; no mass/thrust properties; no environmental interaction

Inputs / Parameters

ParameterValueUnitProvenance
Initial altitude10mDESIGNED
Descent rate1.0m/sDESIGNED

MEASURED = 0 parameters across all 9 technologies. Physical calibration deferred.

Experiment

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What This Result Does Not Prove

This result does NOT prove: transition reliability, mass achievement, hover endurance, ground locomotion capability, or real-world hybrid operation. STATE-MACHINE MODEL ≠ PHYSICAL HYBRID SYSTEM.

Next Research Step

NEXT DIGITAL STEP

Mass and propulsion baseline (weigh-in, thrust stand). Ground locomotion tests. Tethered air mode.

FUTURE PHYSICAL / CALIBRATION STEP

Transition fixture tests (critical gate). Short VLOS flight. Deferred.

Role

FlyScout is a civilian hybrid air/ground reconnaissance micro-drone for infrastructure, agriculture, and environmental monitoring. Explicitly separated from the BW-C45 carrier programme. Campaign C05.

Digital Results

C12 FlyScout state-machine transition model executed. Transition completed successfully. Final state: ground. State-machine model verified. Simulation-only.

Physical Results

No prototype. No mass/thrust measurements. No transition fixture. No CAD/STL for FlyScout.

Proven

C12 state-machine transition model: state sequence verified. Civilian hybrid concept exists. PRE-ALPHA documentation complete. Program explicitly separated from BW-C45.

Not Yet Validated

Transition reliability in hardware (Unknown). Mass achievement (Estimated). TRL >= 3 (not permitted). No physical validation. Hover endurance, ground locomotion, air-ground transition — all unknown. All results state-machine/simulation-only.

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