Objectives:
- Create a Python program to calculate aircraft performance metrics based on user input.
- Incorporate formulas for range, endurance, fuel consumption, and climb performance.
- Allow users to specify aircraft characteristics such as weight, wing area, and engine thrust.
- Provide graphical outputs and analysis of performance trade-offs.
Objectives:
- Develop a minimalist CLI tool to solve International Standard Atmosphere (ISA) equations with high numerical accuracy.
- Implement a stepwise recursive algorithm to handle varying lapse rates across multiple atmospheric layers up to 85,000 meters.
- Calculate critical aeronautical parameters including ambient pressure, temperature, air density, and speed of sound.
- Adhere to "suckless" programming principles by optimizing for execution speed and zero external library dependencies.
GPL-3.0-or-later