Custer UAV Flight Dynamics mathematical model

Custer UAV Flight Dynamics mathematical model as per the PhD thesis, implemented in MATLAB.

call Load_params(1) to load all the Custer UAV parameters and generate plots.

run Run_to_trim.m to generate the trim points along the Custer UAV flight envelope.

run Run_A_and_eigs.m to see the state matrices and generate the eigenvalue plots.

Name		Name	Last commit message	Last commit date
Aero_data_files		Aero_data_files
Aero_data_files2		Aero_data_files2
Aero_data_files3		Aero_data_files3
Aero_data_files4		Aero_data_files4
.gitattributes		.gitattributes
.gitignore		.gitignore
Aero_static_fits.m		Aero_static_fits.m
Cross_Matrix.m		Cross_Matrix.m
Eigenvalues_plot.m		Eigenvalues_plot.m
Extract_aero_states.m		Extract_aero_states.m
Extract_body_states.m		Extract_body_states.m
Forces_and_Moments.asv		Forces_and_Moments.asv
Forces_and_Moments.m		Forces_and_Moments.m
LICENSE		LICENSE
Load_params.m		Load_params.m
Load_params_old.m		Load_params_old.m
ODE_Jac_num.m		ODE_Jac_num.m
ODE_fun.m		ODE_fun.m
README.md		README.md
Rotation_and_Euler_Matrices.m		Rotation_and_Euler_Matrices.m
Run_A_and_eigs.m		Run_A_and_eigs.m
Run_stabilize.m		Run_stabilize.m
Run_stabilize_actuator_c.m		Run_stabilize_actuator_c.m
Run_to_trim.m		Run_to_trim.m
Run_to_trim_old.m		Run_to_trim_old.m
Test_functions.m		Test_functions.m
To_wind_frame.m		To_wind_frame.m
Trim_conditions.m		Trim_conditions.m
Trim_conditions_later.m		Trim_conditions_later.m
Untitled_Aero_Body_conversions.m		Untitled_Aero_Body_conversions.m
Untitled_aero_derivatives_coefs.m		Untitled_aero_derivatives_coefs.m
Untitled_airfoil_rotation.m		Untitled_airfoil_rotation.m
Untitled_control_surf_scaling.asv		Untitled_control_surf_scaling.asv
Untitled_control_surf_scaling.m		Untitled_control_surf_scaling.m
Wind_frame_matrix.m		Wind_frame_matrix.m
bluewhitered.m		bluewhitered.m
ode1.m		ode1.m
startup.m		startup.m

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