F16 Model
This is a simple 13 state model of the F16 flight dynamics. It has 12 rigid
body models plus one mode for the engine. It uses tables for the
aerodynamic coefficients and includes turbulence inputs.
- f16.tar - Unix tar file containing all of the files
necessary to use the model either standalone or within Matlab.
- f16_deq.f - FORTRAN function to compute state derivative
of F16 model. This is the file that actual defines the model and has all of
the aerodynamic coefficients in it.
- f16_massprop.m - Matlab function to compute
pass properties for F16 model. You will need this in order to initialize the
model, even if you aren't using Matlab.
- f16_deqg.F - interface function for matlab (via
fmex).
- f16java.tar - Unix tar file containtint a Java
port of the model, by Ken
Brussel.
Source: NASA TP-1538, December 1979.
Contact: Richard Murray
Additional information
Richard Murray (murray@indra.caltech.edu)
Last modified: Sat Dec 30 18:50:35 1995