Aircraft Control System Design using Linear Inequality Approach
Self-developed aircraft control system implementation employing linear inequality methodology with MATLAB m-file documentation and Simulink model validation for system simulation.
Explore MATLAB source code curated for "飞行器控制系统设计" with clean implementations, documentation, and examples.
Self-developed aircraft control system implementation employing linear inequality methodology with MATLAB m-file documentation and Simulink model validation for system simulation.