HydroSDL/hydro_source/aero_coeff_control.cpp File Reference

#include "math.h"
#include "mex.h"
#include "string.h"
#include "Datas.h"
#include "aero_coeff_control.h"

Include dependency graph for aero_coeff_control.cpp:

Go to the source code of this file.

Defines
#define	pi   3.141592653589793
#define	PI   3.141592653589793
Functions
void	aero_coeff_control (datas *d)
	Aoero/nautical coefficients computing.

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Detailed Description

Author:

basile.graf@epfl.ch

This file contains stuff related to Lift and Drag computation...

Definition in file aero_coeff_control.cpp.

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Define Documentation

#define PI   3.141592653589793

Definition at line 19 of file aero_coeff_control.cpp.

#define pi   3.141592653589793

Definition at line 18 of file aero_coeff_control.cpp.

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Function Documentation

void aero_coeff_control

(

datas *

d

)

Aoero/nautical coefficients computing.

Computes lift and drag coefficients for all surfaces/bodies.
Polynomial forms are used, polar tables are still to be implemented!!

Parameters:

*d

: pointer to the datas data-structure

Definition at line 23 of file aero_coeff_control.cpp.

References datas::A_left, datas::A_pitch, datas::A_right, datas::A_yaw, datas::AR_left, datas::AR_pitch, datas::AR_right, datas::AR_sail, datas::AR_yaw, datas::CD_left, datas::CD_pitch, datas::CD_right, datas::CD_sail, datas::CD_yaw, datas::Chord, datas::Chord_left, datas::Chord_max, datas::Chord_min, datas::Chord_right, datas::CL_left, datas::CL_pitch, datas::CL_right, datas::CL_sail, datas::CL_yaw, datas::E_foils, datas::E_yaw, datas::EE_left, datas::EE_right, datas::EE_yaw, datas::gamma, pi, datas::Tan_AoA_left, datas::Tan_AoA_pitch, datas::Tan_AoA_right, datas::Tan_AoA_sail, and datas::Tan_AoA_yaw.

Referenced by compute_state_dot().

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