Bhaswati23/ADRC-Enabled-6-DOF-Aerospace-Autopilot-Simulator
This work presents a 6-DOF missile guidance and control system integrating Active Disturbance Rejection Control (ADRC) with Proportional Navigation (PN). An Extended State Observer (ESO) is employed to estimate and mitigate disturbances in real time. Simulation data are utilized to train DNN and LSTM models to check tracking trajectory accuracy.
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