Aircraft Weight and Balance Calculator (MATLAB)

This project calculates the weight and balance of an aircraft using given input parameters.
It was developed using MATLAB to apply aerospace engineering concepts related to mass properties and center of gravity analysis.

Project Objective

• Compute aircraft weight and balance
• Calculate air density as a function of altitude
• Perform unit conversions required for flight calculations
• Apply MATLAB programming to aerospace problems

Tools & Language

• MATLAB
• Script-based calculations
• Basic aerospace equations

Files in This Repository

File	Description
WBcalc.m	Main script to compute aircraft weight and balance
DensityAltCalc.m	Calculates air density based on altitude
inputValues.m	Stores user-defined aircraft parameters
kelvinToCelsius.m	Converts temperature from Kelvin to Celsius

How to Run

1. Open MATLAB
2. Set the folder to this repository
3. Run the main script:

WBcalc