About this document
F-16 Trim Analysis Using MATLAB by anees.aero19 is a document available to read on EtoBox.
The document details the stability and trim analysis of the F-16 aircraft, focusing on finding the trim point under specific flight conditions. It includes calculations for trim conditions, optimization using fmincon, and linearization of the dynamics at the equilibrium point. The results include the linearized A and B matrices, which are essential for control design and analysis.
- Author
- anees.aero19
- Language
- EN