Aircraft Climbing Simulation

This simulation program is particularly suitable for individuals seeking to learn aviation principles. The system implements aircraft climbing dynamics through differential equations modeling forces like lift, thrust, drag, and weight. Beyond simulating climb maneuvers, the program generates real-time outputs of critical flight attitudes including pitch, roll, and yaw angles using quaternion-based orientation calculations. These attitude parameters are essential for pilots as they provide crucial information about the aircraft's spatial orientation and directional control. The simulation architecture allows for modular integration of additional flight parameters through configurable input modules - environmental factors such as wind velocity (implemented as vector fields) and air density (modeled using standard atmospheric tables) can be incorporated to enhance realism. The core algorithm employs numerical integration methods (e.g., Runge-Kutta) to solve flight dynamics equations. For those pursuing deeper aviation knowledge, this simulation provides an excellent framework with expandable parameter systems and physically accurate motion models.