06/18/2001 (RD) Added aileron_input, rudder_input,
pilot_elev_no, pilot_ail_no, and
pilot_rud_no
- 11/12/2001 (RD) Added flap_max, flap_rate, and
+ 11/12/2001 (RD) Added flap_max, flap_rate
----------------------------------------------------------------------
AUTHOR(S): Bipin Sehgal <bsehgal@uiuc.edu>
- Jeff Scott <jscott@mail.com>
+ Jeff Scott http://www.jeffscott.net/
Robert Deters <rdeters@uiuc.edu>
----------------------------------------------------------------------
but WITHOUT ANY WARRANTY; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
GNU General Public License for more details.
-
+
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.
+
**********************************************************************/
#include "uiuc_map_controlSurface.h"
controlSurface_map["pilot_elev_no"] = pilot_elev_no_flag ;
controlSurface_map["pilot_ail_no"] = pilot_ail_no_flag ;
controlSurface_map["pilot_rud_no"] = pilot_rud_no_flag ;
+
controlSurface_map["flap_max"] = flap_max_flag ;
controlSurface_map["flap_rate"] = flap_rate_flag ;
+ controlSurface_map["use_flaps"] = use_flaps_flag ;
+
+ controlSurface_map["spoiler_max"] = spoiler_max_flag ;
+ controlSurface_map["spoiler_rate"] = spoiler_rate_flag ;
+ controlSurface_map["use_spoilers"] = use_spoilers_flag ;
+
+ controlSurface_map["gear_max"] = gear_max_flag ;
+ controlSurface_map["gear_rate"] = gear_rate_flag ;
+ controlSurface_map["use_gears"] = use_gear_flag ;
+
+ controlSurface_map["aileron_sas_KP"] = aileron_sas_KP_flag ;
+ controlSurface_map["aileron_sas_max"] = aileron_sas_max_flag ;
+ controlSurface_map["aileron_stick_gain"] = aileron_stick_gain_flag ;
+ controlSurface_map["elevator_sas_KQ"] = elevator_sas_KQ_flag ;
+ controlSurface_map["elevator_sas_max"] = elevator_sas_max_flag ;
+ controlSurface_map["elevator_sas_min"] = elevator_sas_min_flag ;
+ controlSurface_map["elevator_stick_gain"] = elevator_stick_gain_flag ;
+ controlSurface_map["rudder_sas_KR"] = rudder_sas_KR_flag ;
+ controlSurface_map["rudder_sas_max"] = rudder_sas_max_flag ;
+ controlSurface_map["rudder_stick_gain"] = rudder_stick_gain_flag ;
+ controlSurface_map["use_aileron_sas_type1"] = use_aileron_sas_type1_flag ;
+ controlSurface_map["use_elevator_sas_type1"] = use_elevator_sas_type1_flag ;
+ controlSurface_map["use_rudder_sas_type1"] = use_rudder_sas_type1_flag ;
+
+ controlSurface_map["ap_pah"] = ap_pah_flag ;
+ controlSurface_map["ap_alh"] = ap_alh_flag ;
+ controlSurface_map["ap_rah"] = ap_rah_flag ;
+ controlSurface_map["ap_hh"] = ap_hh_flag ;
+ controlSurface_map["ap_Theta_ref"] = ap_Theta_ref_flag ;
+ controlSurface_map["ap_alt_ref"] = ap_alt_ref_flag ;
+ controlSurface_map["ap_Phi_ref"] = ap_Phi_ref_flag ;
+ controlSurface_map["ap_Psi_ref"] = ap_Psi_ref_flag ;
}
// end uiuc_map_controlSurface.cpp