👉 Missile guidance algorithms are sophisticated computational methods that determine the optimal trajectory and control inputs for a missile to accurately reach its target while accounting for various dynamic factors such as wind, gravity, and the missile's own inertia. These algorithms typically fall into two main categories: kinematic and dynamic. Kinematic algorithms, like the Proportional-Directional (PD) method, rely on known missile parameters and initial conditions to predict the trajectory. Dynamic algorithms, such as the Quadratic Trajectory Equations (QTE) and Model Predictive Control (MPC), incorporate real-time sensor data to adjust the missile's path, ensuring precision even in unpredictable environments. Advanced algorithms also employ techniques like Kalman filtering for state estimation and adaptive control to handle uncertainties, making modern missile guidance systems highly effective in achieving their intended targets.
