Mathematics of Moonlander
This section provides an introduction to the mathematical models behind the Moonlander simulation. The aim is to give insight into how thrust, motion, and landing dynamics are calculated.
The content is divided into several focused topics:
Thrust Model
Engine thrust generation and limits
Motion Calculations
Equations of motion and vehicle dynamics
Impact & Structural Integrity
Landing loads and crash conditions
Adaptive Descent Controller
Guidance algorithm for controlled landing
Each subpage contains equations, explanations, and diagrams illustrating the physics and calculations used in the simulation.