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Kami574/AeroMind-Phi4-mini
AeroMind-Phi4-mini is a machine learning model from Kami574. Use it for the machine learning task on the model card, and read the license before you ship it in a product. The card lists the license as apache-2.0.
This model was finetuned and converted to GGUF format using Unsloth.
Downloads · 30 days
107
9% of all-time downloads
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From the Hugging Face model README
This model was finetuned and converted to GGUF format using Unsloth.
Example usage:
llama-cli -hf Kami574/AeroMind-Phi4-mini --jinjallama-mtmd-cli -hf Kami574/AeroMind-Phi4-mini --jinjaPhi-4-mini-instruct.Q8_0.ggufAn Ollama Modelfile is included for easy deployment. This was trained 2x faster with Unsloth <img src="https://raw.githubusercontent.com/unslothai/unsloth/main/images/unsloth%20made%20with%20love.png" width="200"/>
license: apache-2.0 base_model: unsloth/Phi-4-mini-instruct tags:
This model is a fine-tuned version of Phi-4 Mini optimized for high-fidelity aerospace engineering assistance. It was trained on a custom synthetic dataset generating multi-turn, physics-grounded, and mathematically rigorous engineering dialogues across 30 aerospace subdomains.
microsoft/Phi-4-mini-instructThe dataset generation engine executes 1,000 global production iterations distributed uniformly across all 30 aerospace subdomains, yielding ~33–34 multi-turn conversation instances per subdomain (each containing 1 to 3 turn-pairs per instance).
| # | Subdomain Name | Target Instances | Turns / Sample | Est. Total Q&A Pairs |
|---|---|---|---|---|
| 01 | Aerodynamics | 33–34 | 1–3 | ~65–100 |
| 02 | Hypersonic Aerodynamics | 33–34 | 1–3 | ~65–100 |
| 03 | Boundary Layer Transition | 33–34 | 1–3 | ~65–100 |
| 04 | Aeroelasticity | 33–34 | 1–3 | ~65–100 |
| 05 | Structural Health Monitoring | 33–34 | 1–3 | ~65–100 |
| 06 | Composite Materials Engineering | 33–34 | 1–3 | ~65–100 |
| 07 | Rocket Propulsion | 33–34 | 1–3 | ~65–100 |
| 08 | Rocket Nozzle Design | 33–34 | 1–3 | ~65–100 |
| 09 | Turbomachinery | 33–34 | 1–3 | ~65–100 |
| 10 | Spacecraft Thermal Engineering | 33–34 | 1–3 | ~65–100 |
| 11 | Thermal Protection Systems (TPS) | 33–34 | 1–3 | ~65–100 |
| 12 | Atmospheric Re-entry | 33–34 | 1–3 | ~65–100 |
| 13 | Orbital Mechanics | 33–34 | 1–3 | ~65–100 |
| 14 | Space Debris Management | 33–34 | 1–3 | ~65–100 |
| 15 | Satellite Power Systems | 33–34 | 1–3 | ~65–100 |
| 16 | Aircraft Maintenance | 33–34 | 1–3 | ~65–100 |
| 17 | Aircraft Fuel Efficiency | 33–34 | 1–3 | ~65–100 |
| 18 | Aircraft Icing | 33–34 | 1–3 | ~65–100 |
| 19 | Aircraft Design Optimization | 33–34 | 1–3 | ~65–100 |
| 20 | Flight Dynamics and Stability | 33–34 | 1–3 | ~65–100 |
| 21 | High-Temperature Materials Engineering | 33–34 | 1–3 | ~65–100 |
| 22 | Trajectory Optimization | 33–34 | 1–3 | ~65–100 |
| 23 | Space Mission Planning | 33–34 | 1–3 | ~65–100 |
| 24 | Planetary Entry, Descent, and Landing (EDL) | 33–34 | 1–3 | ~65–100 |
| 25 | Wind Tunnel Testing & Experimental Aerodynamics | 33–34 | 1–3 | ~65–100 |
| 26 | Unmanned Aerial Vehicle (UAV) Design | 33–34 | 1–3 | ~65–100 |
| 27 | Air Traffic Management | 33–34 | 1–3 | ~65–100 |
| 28 | Supersonic Inlet Design | 33–34 | 1–3 | ~65–100 |
| 29 | Avionics and Flight Control Systems | 33–34 | 1–3 | ~65–100 |
| 30 | Space Propulsion | 33–34 | 1–3 | ~65–100 |
| Total | All Subdomains Combined | ~1,000 Raw | 1–3 | ~2,000–2,500 Total Q&As |
Note: Exact final count depends on length-validation filtering and duplicate detection performed during post-generation cleaning.
beta_val, crack_length, combustion_instability, etc.) to evaluate physical reasoning.All training examples enforce the following system prompt:
You are a highly advanced aerospace engineering AI assistant. You provide mathematically rigorous, physics-grounded, and safety-critical responses across all aerospace subdomains.