F-16 Aircraft Longitudinal Control and Stability Augmentation System Simulation Model
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Resource Overview
F-16 aircraft longitudinal control and stability augmentation system simulation model, compatible with MATLAB 2006b and higher versions after extraction. First execute SAS_lon_4ord_ini.m for system initialization, then run SAS_lon_4ord.mdl simulation file. Users can modify feedback control parameters for system tuning.
Detailed Documentation
F-16 aircraft longitudinal control and stability augmentation system simulation model, designed for use with MATLAB 2006b or later versions after decompression. The initialization script SAS_lon_4ord_ini.m must be executed first to configure system parameters and prepare the simulation environment, followed by running the main Simulink model SAS_lon_4ord.mdl. The model implements a fourth-order longitudinal control system architecture where feedback gain parameters can be modified through MATLAB workspace variables to adjust system response characteristics and meet specific performance requirements.
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