Helicopter Sliding Mode Backstepping Control Based on Nonlinear Disturbance Observer
Advanced helicopter control methodology integrating nonlinear disturbance observer with sliding mode and backstepping controllers for robust performance enhancement
Explore MATLAB source code curated for "直升机" with clean implementations, documentation, and examples.
Advanced helicopter control methodology integrating nonlinear disturbance observer with sliding mode and backstepping controllers for robust performance enhancement
A neural network PID control implementation example for helicopter pitch angle control, using a second-order transfer function as the plant model, with code structure and implementation approach explanations.
PID control algorithm for helicopter's three attitude angles using MATLAB/Simulink simulation, integrated with optimal PID design methods to achieve excellent control performance. The implementation includes detailed modeling of roll, pitch, and yaw angles with systematic tuning approaches.
Implementation code for extracting cricket sounds from mixed audio containing both cricket chirps and helicopter noise, along with separated audio files for cricket sounds and helicopter sounds after extraction.