Simulation
The Moonlander simulation models the vertical descent of a lunar lander using a modular C++ backend and a real-time Qt-based visualization frontend. The current implementation demonstrates stable and reproducible one-dimensional landing dynamics.
Demonstration
The following excerpt illustrates a representative simulation run, including altitude, velocity and thrust response over time.
Architecture & Data Flow
The simulation core is implemented in C++ and separated from the visualization layer through a well-defined interface.
- C++ physics core (state propagation and control)
- Interface layer for telemetry exchange
- Qt frontend for real-time visualization
Model Scope & Assumptions
- One-dimensional vertical motion
- Constant lunar gravity
- Discrete-time integration
- Deterministic control input
A detailed mathematical formulation is provided in the Mathematics section.
Stability & Validation
The simulation exhibits stable numerical behavior across multiple runs and serves as a foundation for future extensions toward multi-dimensional dynamics and closed-loop control.