From: <sv...@ww...> - 2005-02-21 23:59:39
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Author: mkrose Date: 2005-02-21 15:59:31 -0800 (Mon, 21 Feb 2005) New Revision: 1484 Modified: trunk/CSP/CSPSim/CHANGES.current trunk/CSP/CSPSim/Data/XML/vehicles/aircraft/m2k/fm.xml Log: * Fix rudder yaw coefficients; new values work for rudder angle in radians. * Increase rudder yaw moment (cn_dr). The new coefficient is the nominal F-16 value, which matches the lateral force coefficient. If this value needs to be decrease then cy_r should be decreased as well. * Similar fixes need to be applied to the f-16 fm (which is just a copy of the m2k fm right now). I'm working on more substantial changes to that fm so I'll leave it as is for now. Browse at: https://www.zerobar.net/viewcvs/viewcvs.cgi?view=rev&rev=1484 Modified: trunk/CSP/CSPSim/CHANGES.current =================================================================== --- trunk/CSP/CSPSim/CHANGES.current 2005-02-21 23:03:53 UTC (rev 1483) +++ trunk/CSP/CSPSim/CHANGES.current 2005-02-21 23:59:31 UTC (rev 1484) @@ -1,20 +1,31 @@ Version 0.4.0 (in progress) =========================== +2005-02-21: onsight + * Fix rudder yaw coefficients; new values work for rudder angle in radians. + + * Increase rudder yaw moment (cn_dr). The new coefficient is the nominal + F-16 value, which matches the lateral force coefficient. If this value + needs to be decrease then cy_r should be decreased as well. + + * Similar fixes need to be applied to the f-16 fm (which is just a copy of + the m2k fm right now). I'm working on more substantial changes to that + fm so I'll leave it as is for now. + 2005-02-21: delta * Minor change to the m2k model to correctly retract the right gear. - + * Minor patch to CSPSim.py to execute cspinput in case an hid file is missing. cspinput is not an executable on windows and must be called as an argument of python(.exe). Should be checked on GNU/Linux to be sure it doesn't break the stuff there. - + 2005-02-21: lologramme * Add Light pylons in the hangars area. - + 2005-02-20: onsight * Fix path for hid generation under windows. - + * Add the correct F16DJ binding for the core aircraft.map. 2005-02-18: delta Modified: trunk/CSP/CSPSim/Data/XML/vehicles/aircraft/m2k/fm.xml =================================================================== --- trunk/CSP/CSPSim/Data/XML/vehicles/aircraft/m2k/fm.xml 2005-02-21 23:03:53 UTC (rev 1483) +++ trunk/CSP/CSPSim/Data/XML/vehicles/aircraft/m2k/fm.xml 2005-02-21 23:59:31 UTC (rev 1484) @@ -106,23 +106,26 @@ <Float name="cy_dr">-0.15</Float> <Table2 name="cy_m_a"> <Breaks0 spacing="0.1"> + <!-- mach --> 0.0 0.5 0.7 0.8 0.9 1.0 1.2 1.4 2.0 2.5 </Breaks0> <Breaks1 spacing="0.01"> + <!-- alpha in radians --> -0.34906585 -0.174532925 -0.087266463 0.0 0.087266463 0.13962634 0.20943951 0.296705973 0.34906585 0.436332313 0.523598776 0.698131701 1.047197551 </Breaks1> <Values> - -0.0109 -0.0166 -0.0182 -0.0192 -0.0192 -0.0187 -0.0163 -0.0176 -0.0164 -0.0158 -0.0141 -0.009 -0.011 - -0.0109 -0.0166 -0.0182 -0.0192 -0.0192 -0.0187 -0.0163 -0.0176 -0.0164 -0.0158 -0.0141 -0.009 -0.016 - -0.0109 -0.0166 -0.0182 -0.0192 -0.0192 -0.0187 -0.0163 -0.0176 -0.0164 -0.0158 -0.0141 -0.009 -0.016 - -0.0122 -0.021 -0.028 -0.0286 -0.0286 -0.03 -0.025 -0.0267 -0.0223 -0.0215 -0.0187 -0.0172 -0.017 - -0.0172 -0.027 -0.033 -0.035 -0.035 -0.033 -0.0321 -0.0288 -0.0254 -0.0231 -0.0207 -0.0188 -0.0171 - -0.01725 -0.0271 -0.03325 -0.03525 -0.03525 -0.03355 -0.03235 -0.029 -0.0257 -0.02355 -0.02085 -0.0194 -0.01715 - -0.017275 -0.02715 -0.033375 -0.035375 -0.035375 -0.033675 -0.032475 0 -0.02585 -0.023775 -0.020925 -0.0197 -0.0172 - -0.0173 -0.0272 -0.0335 -0.0355 -0.0355 -0.0338 -0.0326 -0.0292 -0.026 -0.024 -0.021 -0.02 -0.0172 - -0.0173 -0.0272 -0.0335 -0.0355 -0.0355 -0.0338 -0.0326 -0.0292 -0.026 -0.024 -0.021 -0.02 -0.0161 - -0.0162 -0.0194 -0.0194 -0.0215 -0.0215 -0.0216 -0.0214 -0.0215 -0.0205 -0.0179 -0.0153 -0.0105 1 + <!-- coefficients assuming rudder deflection is in radians --> + -0.625 -0.951 -1.043 -1.100 -1.100 -1.071 -0.934 -1.008 -0.940 -0.905 -0.808 -0.516 -0.630 + -0.625 -0.951 -1.043 -1.100 -1.100 -1.071 -0.934 -1.008 -0.940 -0.905 -0.808 -0.516 -0.917 + -0.625 -0.951 -1.043 -1.100 -1.100 -1.071 -0.934 -1.008 -0.940 -0.905 -0.808 -0.516 -0.917 + -0.699 -1.203 -1.604 -1.639 -1.639 -1.719 -1.432 -1.530 -1.278 -1.232 -1.071 -0.985 -0.974 + -0.985 -1.547 -1.891 -2.005 -2.005 -1.891 -1.839 -1.650 -1.455 -1.324 -1.186 -1.077 -0.980 + -0.988 -1.553 -1.905 -2.020 -2.020 -1.922 -1.854 -1.662 -1.473 -1.349 -1.195 -1.112 -0.983 + -0.990 -1.556 -1.912 -2.027 -2.027 -1.929 -1.861 -0.000 -1.481 -1.362 -1.199 -1.129 -0.985 + -0.991 -1.558 -1.919 -2.034 -2.034 -1.937 -1.868 -1.673 -1.490 -1.375 -1.203 -1.146 -0.985 + -0.991 -1.558 -1.919 -2.034 -2.034 -1.937 -1.868 -1.673 -1.490 -1.375 -1.203 -1.146 -0.922 + -0.928 -1.112 -1.112 -1.232 -1.232 -1.238 -1.226 -1.232 -1.175 -1.026 -0.877 -0.602 -0.573 </Values> </Table2> @@ -144,6 +147,7 @@ <!--Float name="cn_r">-8.17</Float--><!-- <0 --> <Float name="cn_r">-16</Float><!-- <0 --> <Float name="cn_da">-0.0747</Float> - <Float name="cn_dr">0.0293</Float> + <!-- CHECK: this is the (nominal) F16 value, previously was set to 0.0293 --> + <Float name="cn_dr">0.086</Float> </Object> |