----------------------------------------------------------------------
HISTORY: 04/15/2000 initial release
+ 10/25/2001 (RD) Added new variables needed for the non-
+ linear Twin Otter model at zero flaps
+ (Cnfxxf0)
+ 11/12/2001 (RD) Added new variables needed for the non-
+ linear Twin Otter model with flaps
+ (Cnfxxf). Zero flap vairables removed.
+ 02/13/2002 (RD) Added variables so linear aero model
+ values can be recorded
+ 02/18/2002 (RD) Added uiuc_3Dinterp_quick() function
+ for a quicker 3D interpolation. Takes
+ advantage of "nice" data.
----------------------------------------------------------------------
AUTHOR(S): Bipin Sehgal <bsehgal@uiuc.edu>
Jeff Scott <jscott@mail.com>
+ Robert Deters <rdeters@uiuc.edu>
----------------------------------------------------------------------
CALLS TO: uiuc_1Dinterpolation
uiuc_2Dinterpolation
uiuc_ice_filter
+ uiuc_3Dinterpolation
+ uiuc_3Dinterp_quick
----------------------------------------------------------------------
You should have received a copy of the GNU General Public License
along with this program; if not, write to the Free Software
- Foundation, Inc., 59 Temple Place - Suite 330, Boston, MA 02111-1307,
- USA or view http://www.gnu.org/copyleft/gpl.html.
+ Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA 02110-1301, USA.
**********************************************************************/
string linetoken1;
string linetoken2;
stack command_list;
-
+
+ double p_nondim;
+ double r_nondim;
+
command_list = aeroYawParts -> getCommands();
for (LIST command_line = command_list.begin(); command_line!=command_list.end(); ++command_line)
{
Cno = uiuc_ice_filter(Cno_clean,kCno);
}
- Cn += Cno;
+ Cno_save = Cno;
+ Cn += Cno_save;
break;
}
case Cn_beta_flag:
{
Cn_beta = uiuc_ice_filter(Cn_beta_clean,kCn_beta);
}
- Cn += Cn_beta * Beta;
+ Cn_beta_save = Cn_beta * Std_Beta;
+ if (eta_q_Cn_beta_fac)
+ {
+ Cn += Cn_beta_save * eta_q_Cn_beta_fac;
+ }
+ else
+ {
+ Cn += Cn_beta_save;
+ }
break;
}
case Cn_p_flag:
}
/* Cn_p must be mulitplied by b/2U
(see Roskam Control book, Part 1, pg. 147) */
- Cn += Cn_p * P_body * b_2U;
+ Cn_p_save = Cn_p * P_body * b_2U;
+ if (eta_q_Cn_p_fac)
+ {
+ Cn += Cn_p_save * eta_q_Cn_p_fac;
+ }
+ else
+ {
+ Cn += Cn_p_save;
+ }
break;
}
case Cn_r_flag:
}
/* Cn_r must be mulitplied by b/2U
(see Roskam Control book, Part 1, pg. 147) */
- Cn += Cn_r * R_body * b_2U;
+ Cn_r_save = Cn_r * R_body * b_2U;
+ if (eta_q_Cn_r_fac)
+ {
+ Cn += Cn_r_save * eta_q_Cn_r_fac;
+ }
+ else
+ {
+ Cn += Cn_r_save;
+ }
break;
}
case Cn_da_flag:
{
Cn_da = uiuc_ice_filter(Cn_da_clean,kCn_da);
}
- Cn += Cn_da * aileron;
+ Cn_da_save = Cn_da * aileron;
+ Cn += Cn_da_save;
break;
}
case Cn_dr_flag:
{
Cn_dr = uiuc_ice_filter(Cn_dr_clean,kCn_dr);
}
- Cn += Cn_dr * rudder;
+ Cn_dr_save = Cn_dr * rudder;
+ if (eta_q_Cn_dr_fac)
+ {
+ Cn += Cn_dr_save * eta_q_Cn_dr_fac;
+ }
+ else
+ {
+ Cn += Cn_dr_save;
+ }
break;
}
case Cn_q_flag:
{
Cn_q = uiuc_ice_filter(Cn_q_clean,kCn_q);
}
- Cn += Cn_q * Q_body * cbar_2U;
+ Cn_q_save = Cn_q * Q_body * cbar_2U;
+ Cn += Cn_q_save;
break;
}
case Cn_b3_flag:
{
Cn_b3 = uiuc_ice_filter(Cn_b3_clean,kCn_b3);
}
- Cn += Cn_b3 * Beta * Beta * Beta;
+ Cn_b3_save = Cn_b3 * Std_Beta * Std_Beta * Std_Beta;
+ Cn += Cn_b3_save;
break;
}
case Cnfada_flag:
Cnfada_CnArray,
Cnfada_nAlphaArray,
Cnfada_nda,
- Alpha,
+ Std_Alpha,
aileron);
Cn += CnfadaI;
break;
Cnfbetadr_CnArray,
Cnfbetadr_nBetaArray,
Cnfbetadr_ndr,
- Beta,
+ Std_Beta,
rudder);
Cn += CnfbetadrI;
break;
}
+ case Cnfabetaf_flag:
+ {
+ if (Cnfabetaf_nice == 1)
+ CnfabetafI = uiuc_3Dinterp_quick(Cnfabetaf_fArray,
+ Cnfabetaf_aArray_nice,
+ Cnfabetaf_bArray_nice,
+ Cnfabetaf_CnArray,
+ Cnfabetaf_na_nice,
+ Cnfabetaf_nb_nice,
+ Cnfabetaf_nf,
+ flap_pos,
+ Std_Alpha,
+ Std_Beta);
+ else
+ CnfabetafI = uiuc_3Dinterpolation(Cnfabetaf_fArray,
+ Cnfabetaf_aArray,
+ Cnfabetaf_betaArray,
+ Cnfabetaf_CnArray,
+ Cnfabetaf_nAlphaArray,
+ Cnfabetaf_nbeta,
+ Cnfabetaf_nf,
+ flap_pos,
+ Std_Alpha,
+ Std_Beta);
+ Cn += CnfabetafI;
+ break;
+ }
+ case Cnfadaf_flag:
+ {
+ if (Cnfadaf_nice == 1)
+ CnfadafI = uiuc_3Dinterp_quick(Cnfadaf_fArray,
+ Cnfadaf_aArray_nice,
+ Cnfadaf_daArray_nice,
+ Cnfadaf_CnArray,
+ Cnfadaf_na_nice,
+ Cnfadaf_nda_nice,
+ Cnfadaf_nf,
+ flap_pos,
+ Std_Alpha,
+ aileron);
+ else
+ CnfadafI = uiuc_3Dinterpolation(Cnfadaf_fArray,
+ Cnfadaf_aArray,
+ Cnfadaf_daArray,
+ Cnfadaf_CnArray,
+ Cnfadaf_nAlphaArray,
+ Cnfadaf_nda,
+ Cnfadaf_nf,
+ flap_pos,
+ Std_Alpha,
+ aileron);
+ Cn += CnfadafI;
+ break;
+ }
+ case Cnfadrf_flag:
+ {
+ if (Cnfadrf_nice == 1)
+ CnfadrfI = uiuc_3Dinterp_quick(Cnfadrf_fArray,
+ Cnfadrf_aArray_nice,
+ Cnfadrf_drArray_nice,
+ Cnfadrf_CnArray,
+ Cnfadrf_na_nice,
+ Cnfadrf_ndr_nice,
+ Cnfadrf_nf,
+ flap_pos,
+ Std_Alpha,
+ rudder);
+ else
+ CnfadrfI = uiuc_3Dinterpolation(Cnfadrf_fArray,
+ Cnfadrf_aArray,
+ Cnfadrf_drArray,
+ Cnfadrf_CnArray,
+ Cnfadrf_nAlphaArray,
+ Cnfadrf_ndr,
+ Cnfadrf_nf,
+ flap_pos,
+ Std_Alpha,
+ rudder);
+ Cn += CnfadrfI;
+ break;
+ }
+ case Cnfapf_flag:
+ {
+ p_nondim = P_body * b_2U;
+ if (Cnfapf_nice == 1)
+ CnfapfI = uiuc_3Dinterp_quick(Cnfapf_fArray,
+ Cnfapf_aArray_nice,
+ Cnfapf_pArray_nice,
+ Cnfapf_CnArray,
+ Cnfapf_na_nice,
+ Cnfapf_np_nice,
+ Cnfapf_nf,
+ flap_pos,
+ Std_Alpha,
+ p_nondim);
+ else
+ CnfapfI = uiuc_3Dinterpolation(Cnfapf_fArray,
+ Cnfapf_aArray,
+ Cnfapf_pArray,
+ Cnfapf_CnArray,
+ Cnfapf_nAlphaArray,
+ Cnfapf_np,
+ Cnfapf_nf,
+ flap_pos,
+ Std_Alpha,
+ p_nondim);
+ Cn += CnfapfI;
+ break;
+ }
+ case Cnfarf_flag:
+ {
+ r_nondim = R_body * b_2U;
+ if (Cnfarf_nice == 1)
+ CnfarfI = uiuc_3Dinterp_quick(Cnfarf_fArray,
+ Cnfarf_aArray_nice,
+ Cnfarf_rArray_nice,
+ Cnfarf_CnArray,
+ Cnfarf_na_nice,
+ Cnfarf_nr_nice,
+ Cnfarf_nf,
+ flap_pos,
+ Std_Alpha,
+ r_nondim);
+ else
+ CnfarfI = uiuc_3Dinterpolation(Cnfarf_fArray,
+ Cnfarf_aArray,
+ Cnfarf_rArray,
+ Cnfarf_CnArray,
+ Cnfarf_nAlphaArray,
+ Cnfarf_nr,
+ Cnfarf_nf,
+ flap_pos,
+ Std_Alpha,
+ r_nondim);
+ Cn += CnfarfI;
+ break;
+ }
};
} // end Cn map
projects / flightgear.git / blobdiff