A3M35SRL - Systémy řízení letu, Control systems for aircraft and spacecraft
The course is devoted to classical and modern control design techniques for autopilots and flight control systems Particular levels are discussed, starting with the dampers attitude angle stabilizers, to guidance and navigation systems. Next to the design itself, important aspects of aircraft modelling, both as a rigid body and considering flexibility of the structure, are discussed.
Výsledek studentské ankety předmětu je zde: A3M35SRL
Nonlinear F-16 model for the semester project. Includes all necessary files. MATLAB requires a mex computer to run nlplant.c.
Test your mex compiler by typing the following into the MATLAB command window:
mex -setup
Updates:
- graphF16.m fixed for running lo-fidelity model