[Csp-commits] APPLICATIONS/CSPFlightSim/scripts AeroM2k.csp,1.2,1.3

[<mk...@us...>]

Update of /cvsroot/csp/APPLICATIONS/CSPFlightSim/scripts
In directory sc8-pr-cvs1:/tmp/cvs-serv28509/CSPFlightSim/scripts

Modified Files:
	AeroM2k.csp 
Log Message:
fixed a couple build dependencies, related to osg cvs (should still work with osg 0.9.2)
flight model parameters for M2k updated from delta

Index: AeroM2k.csp
===================================================================
RCS file: /cvsroot/csp/APPLICATIONS/CSPFlightSim/scripts/AeroM2k.csp,v
retrieving revision 1.2
retrieving revision 1.3
diff -C2 -d -r1.2 -r1.3
*** AeroM2k.csp	5 Dec 2002 04:09:41 -0000	1.2
--- AeroM2k.csp	13 Dec 2002 01:20:59 -0000	1.3
***************
*** 1,81 ****
! REM Mirage 2000 aerodynamics model
! REM many parameters are estimates.
! 
! Add Aero M2K_aero
! 
! REM Wing geometry
! set M2K_aero WingSpan 9.13
! set M2K_aero WingChord 4.5
! set M2K_aero WingArea 41.0
! 
! REM Control surfaces min/max angles
! Set M2K_aero demax        25.0
! Set M2K_aero demin        -16.0
! Set M2K_aero damax        +17.5
! Set M2K_aero damin        -17.5
! Set M2K_aero drmax        +20.0
! Set M2K_aero drmin        -20.0
! 
! REM A=0.9 10^4 kg m²       A -F -E
! REM C=6.0 10^4 kg m²  I = -F  B -D
! REM B=5.4 10^4 Kg m²      -E -D  C
! REM E=1.8 10^3 kg m²
! 
! REM Mass/Inertial properties
! REM max mass
! REM Set M2K_aero Mass         17500.0
! REM interceptor mass with a central tank
! Set M2K_aero Mass         12000.0
! REM interceptor mass
! REM Set M2K_aero Mass         7500.0
! 
! Set M2K_aero I_XX        20354.0
! Set M2K_aero I_YY        135691.0
! Set M2K_aero I_ZZ        135691.0
! Set M2K_aero I_XZ         6785.0
! 
! Set M2K_aero GMIN      -3.0
! Set M2K_aero GMAX       9.0
! 
! Set M2K_aero ThrustMax 9700.0
! 
! REM Drag Parameters cx0 = 2 *  0.074 / ( rc^0.2 ) ; Cx=Cx0+KiCz² Ki(trainee induite) 1/pi*AR
! Set M2K_aero CD0          0.004
! Set M2K_aero CD_a         0.3
! Set M2K_aero CD_de        0.1
! 
! REM Lift Parameters
! Set M2K_aero StallAOA     31.0
! Set M2K_aero CL0          0.0
! Set M2K_aero CL_a         2.2
! Set M2K_aero CL_adot      0.01
! Set M2K_aero CL_q         0.1
! Set M2K_aero CL_de        0.7
! 
! REM Pitch Moment Parameters
! Set M2K_aero CM0          0.0
! Set M2K_aero CM_a         -0.38
! Set M2K_aero CM_adot      -1.1
! Set M2K_aero CM_q         -3.6
! Set M2K_aero CM_de        0.05
! 
! REM Side Force Parameters
! Set M2K_aero CY_Beta      -0.98
! Set M2K_aero CY_p          0.0
! Set M2K_aero CY_r          0.0
! Set M2K_aero CY_da         0.0
! Set M2K_aero CY_dr         0.05
! 
! REM Roll moment parameters
! Set M2K_aero CI_beta       -0.12
! Set M2K_aero CI_p          -0.26
! Set M2K_aero CI_r           0.14
! Set M2K_aero CI_da         0.02
! Set M2K_aero CI_dr         -0.001
! 
! Rem Yaw Moment Parameters
! Set M2K_aero Cn_beta       0.25
! Set M2K_aero Cn_p          0.022
! Set M2K_aero Cn_r          -0.35
! Set M2K_aero Cn_da         0.00
! Set M2K_aero Cn_dr         0.01
--- 1,81 ----
! REM Mirage 2000 aerodynamics model
! REM many parameters are estimates.
! 
! Add Aero M2K_aero
! 
! REM Wing geometry
! set M2K_aero WingSpan 9.13
! set M2K_aero WingChord 4.5
! set M2K_aero WingArea 41.0
! 
! REM Control surfaces min/max angles
! Set M2K_aero demax        25.0
! Set M2K_aero demin        -16.0
! Set M2K_aero damax        +17.5
! Set M2K_aero damin        -17.5
! Set M2K_aero drmax        +20.0
! Set M2K_aero drmin        -20.0
! 
! REM A=0.9 10^4 kg m²       A -F -E
! REM C=6.0 10^4 kg m²  I = -F  B -D
! REM B=5.4 10^4 Kg m²      -E -D  C
! REM E=1.8 10^3 kg m²
! 
! REM Mass/Inertial properties
! REM max mass
! REM Set M2K_aero Mass         17500.0
! REM interceptor mass with a central tank
! Set M2K_aero Mass         12000.0
! REM interceptor mass
! REM Set M2K_aero Mass         7500.0
! 
! Set M2K_aero I_XX        20354.0
! Set M2K_aero I_YY        135691.0
! Set M2K_aero I_ZZ        135691.0
! Set M2K_aero I_XZ         6785.0
! 
! Set M2K_aero GMIN      -3.0
! Set M2K_aero GMAX       9.0
! 
! Set M2K_aero ThrustMax 9700.0
! 
! REM Drag Parameters cx0 = 2 *  0.074 / ( rc^0.2 ) ; Cx=Cx0+KiCz² Ki(trainee induite) 1/pi*AR
! Set M2K_aero CD0          0.01
! Set M2K_aero CD_a         0.3
! Set M2K_aero CD_de        0.02
! 
! REM Lift Parameters
! Set M2K_aero StallAOA     31.0
! Set M2K_aero CL0          0.0
! Set M2K_aero CL_a         2.2
! Set M2K_aero CL_adot      1.29
! Set M2K_aero CL_q         1.5
! Set M2K_aero CL_de        0.7
! 
! REM Pitch Moment Parameters
! Set M2K_aero CM0          0.0
! Set M2K_aero CM_a         -0.38
! Set M2K_aero CM_adot      -1.73
! Set M2K_aero CM_q         -3.6
! Set M2K_aero CM_de        0.48
! 
! REM Side Force Parameters
! Set M2K_aero CY_Beta      -0.29
! Set M2K_aero CY_p          0.11
! Set M2K_aero CY_r          0.0
! Set M2K_aero CY_da         0.0
! REM Set M2K_aero CY_dr         -0.01
! 
! REM Roll moment parameters
! Set M2K_aero CI_beta       -0.17
! Set M2K_aero CI_p          -0.3
! Set M2K_aero CI_r           0.3
! Set M2K_aero CI_da          0.03
! Set M2K_aero CI_dr          0.0
! 
! Rem Yaw Moment Parameters
! Set M2K_aero Cn_beta       0.25
! Set M2K_aero Cn_p          0.0
! Set M2K_aero Cn_r          -0.99
! Set M2K_aero Cn_da         0.00
! Set M2K_aero Cn_dr         0.02