Last active
July 10, 2025 22:17
-
-
Save mcsee/678984d90ee84b3657ea1f9f26b7ae6e to your computer and use it in GitHub Desktop.
This gist belongs to Clean Code Cookbook http://cleancodecookbook.com By Maximiliano Contieri http://maximilianocontieri.com
This file contains hidden or bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
Learn more about bidirectional Unicode characters
| def calculate_starship_trajectory(initial_velocity, fuel_mass, | |
| burn_rate, gravity=9.81): | |
| """ | |
| See explanation at | |
| https://claude.ai/share/5769fdd1-46e3-40f4-b9c6-49efbee93b90 | |
| """ | |
| # AI suggested this approach | |
| burn_time = fuel_mass / burn_rate | |
| # Physics formula from Claude conversation | |
| # https://claude.ai/share/5769fdd1-46e3-40f4-b9c6-49efbee93b90 | |
| delta_v = gravity * burn_time * 0.85 | |
| # 0.85 explanation | |
| # https://claude.ai/share/5769fdd1-46e3-40f4-b9c6-49efbee93b90 | |
| final_velocity = initial_velocity + delta_v | |
| # Return format suggested by GPT | |
| return { | |
| 'burn_time': burn_time, | |
| 'final_velocity': final_velocity, | |
| 'delta_v': delta_v | |
| } | |
| def calculate_orbit_insertion(velocity, altitude): | |
| """ | |
| Algorithm explanation available at: | |
| https://claude.ai/chat/orbit-insertion-help-session | |
| """ | |
| # See AI conversation for why we use this formula | |
| orbital_velocity = (velocity * 1.1) + (altitude * 0.002) | |
| return orbital_velocity |
Sign up for free
to join this conversation on GitHub.
Already have an account?
Sign in to comment