LAB 2: Spring-Mass-Damper (Aircraft Landing Gear) Using Matlab/imulink

AIM OF THE EXPERIMENT
To study the dynamic behavior of a spring–mass–damper system and investigate the effects of underdamping, critical damping, and overdamping using MATLAB/Simulink.

OBJECTIVES
1. To model a spring–mass–damper system in Simulink.
2. To observe oscillatory motion under different damping conditions.
3. To compare underdamped, critically damped, and overdamped responses.
4. To understand the role of damping in aircraft landing gear systems.
5. To determine the effect of damping coefficient on system stability.

Видео LAB 2: Spring-Mass-Damper (Aircraft Landing Gear) Using Matlab/imulink канала Abbas Abdullahi