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Commit fface08

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author
Luiz Renault
committed
Mostly A/G mode implementations
1 parent b348e8b commit fface08

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17 files changed

+571
-507
lines changed

17 files changed

+571
-507
lines changed

‎A-29B.lua‎

Lines changed: 16 additions & 14 deletions
Original file line numberDiff line numberDiff line change
@@ -262,6 +262,7 @@ A_29B = {
262262
{
263263
{ CLSID = "{6CEB49FC-DED8-4DED-B053-E1F033FF72D3}" }, -- AIM-9P
264264

265+
{ CLSID = "{BCE4E030-38E9-423E-98ED-24BE3DA87C32}" }, -- Mk-82
265266
{ CLSID = "{DB769D48-67D7-42ED-A2BE-108D566C8B1E}" }, --GBU12
266267
{ CLSID = "{0D33DDAE-524F-4A4E-B5B8-621754FE3ADE}" }, --GBU16
267268
{ CLSID = "{5335D97A-35A5-4643-9D9B-026C75961E52}" }, -- CBU-97
@@ -344,6 +345,7 @@ A_29B = {
344345
{
345346
{ CLSID = "{6CEB49FC-DED8-4DED-B053-E1F033FF72D3}" }, -- AIM-9P
346347

348+
{ CLSID = "{BCE4E030-38E9-423E-98ED-24BE3DA87C32}" }, -- Mk-82
347349
{ CLSID = "{DB769D48-67D7-42ED-A2BE-108D566C8B1E}" }, --GBU12
348350
{ CLSID = "{0D33DDAE-524F-4A4E-B5B8-621754FE3ADE}" }, --GBU16
349351
{ CLSID = "{5335D97A-35A5-4643-9D9B-026C75961E52}" }, -- CBU-97
@@ -395,8 +397,8 @@ A_29B = {
395397
{
396398
Cy0 = 0.1, -- Coefficient of lift at zero angle of attack -- Always 0 for symmetrical airfoil
397399
Mzalfa = 4.355, -- Horizontal tail pitch coefficient
398-
Mzalfadt = 0.8, -- Wing pitch coefficient
399-
kjx = 2.25, -- Roll rate acceleration constant in radians / second -- Inertia parametre X - Dimension (clean) airframe drag coefficient at X (Top) Simply the wing area in square meters (as that is a major factor in drag calculations) - smaller = massive inertia
400+
Mzalfadt = 1, -- Wing pitch coefficient
401+
kjx = 2.95, -- Roll rate acceleration constant in radians / second -- Inertia parametre X - Dimension (clean) airframe drag coefficient at X (Top) Simply the wing area in square meters (as that is a major factor in drag calculations) - smaller = massive inertia
400402
kjz = 0.00125, -- Unknown pitch constant. All planes use 0.00125 -- -- Inertia parametre Z - Dimension (clean) airframe drag coefficient at Z (Front) Simply the wing area in square meters (as that is a major factor in drag calculations)
401403
Czbe = -0.016, -- Directional stability coefficient -- coefficient, along Z axis (perpendicular), affects yaw, negative value means force orientation in FC coordinate system
402404
cx_gear = 0.0277, -- Additional coefficient of drag for gear extended
@@ -445,14 +447,14 @@ A_29B = {
445447
-- M Cx0 Cya B B4 Omxmax Aldop Cymax
446448
{-0.1, 0.0187, 0.0746*2, 0.052, 0.012, 0.79, 22.0, 1.45*2, },
447449
{0.0, 0.0187, 0.0746*2, 0.052, 0.012, 0.79, 22.0, 1.45*2, },
448-
{0.2, 0.0187, 0.0746*2, 0.052, 0.012, 0.796144, 22.0, 1.45*2, },
449-
{0.3, 0.0187, 0.0722*2, 0.052, 0.015, 1.24, 19.0, 1.2*2, },
450-
{0.5, 0.0187, 0.0798*2, 0.045, 0.025, 1.323, 17.0, 1.08*2, },
451-
{0.59, 0.0187, 0.084*2, 0.047, 0.026, 1.129077, 17.0, 1.07*2, },
452-
{0.67, 0.0187, 0.0907*2, 0.047, 0.021, 0.943, 14.5, 0.98*2, },
453-
{0.74, 0.0227, 0.0855*2, 0.08, 0.16, 0.675, 10.0, 0.72*2, },
454-
{0.76, 0.032, 0.078*2, 0.1, 0.25, 0.577, 9.0, 0.6*2, },
455-
{0.8, 0.063, 0.072*2, 0.2, 0.36, 0.456, 6.0, 0.4*2, },
450+
{0.2, 0.0187, 0.0746*2, 0.052, 0.012, 2.796144, 22.0, 1.45*2, },
451+
{0.3, 0.0187, 0.0722*2, 0.052, 0.015, 4.24, 19.0, 1.2*2, },
452+
{0.5, 0.0187, 0.0798*2, 0.045, 0.025, 4.323, 17.0, 1.08*2, },
453+
{0.59, 0.0187, 0.084*2, 0.047, 0.026, 4.129077, 17.0, 1.07*2, },
454+
{0.67, 0.0187, 0.0907*2, 0.047, 0.021, 3.943, 14.5, 0.98*2, },
455+
{0.74, 0.0227, 0.0855*2, 0.08, 0.16, 3.675, 10.0, 0.72*2, },
456+
{0.76, 0.032, 0.078*2, 0.1, 0.25, 2.577, 9.0, 0.6*2, },
457+
{0.8, 0.063, 0.072*2, 0.2, 0.36, 1.456, 6.0, 0.4*2, },
456458
{0.83, 0.1, 0.0725*2, 0.34, 2.4, 0.32, 4.5, 0.3*2, },
457459
{0.9, 0.126, 0.073*2, 0.56, 3.0, 0.076, 3.0, 0.2*2, },
458460
{1.1, 0.16, 0.03*2, 0.56, 3.0, 0.076, 1.0, 0.3*2 },
@@ -468,8 +470,8 @@ A_29B = {
468470
typeng = 3, -- E_TURBOJET = 0, E_TURBOJET_AB = 1, E_PISTON = 2, E_TURBOPROP = 3, E_TURBOFAN = 4, E_TURBOSHAFT = 5
469471
hMaxEng = 19.5, -- maximum operating altitude for the engine in km -- typically higher than service ceiling of the aircraft
470472
dcx_eng = 0.0114, -- drag coefficient for the engine -- no correlation found -- most common values are 0.0085 and 0.0144
471-
cemax = 0.097, -- kg / sec - fuel consumption for a single engine in dry configuration
472-
cefor = 0.097, -- kg / sec - fuel consumption for a single engine in afterburner configuration
473+
cemax = 0.0225, -- kg / sec - fuel consumption for a single engine in dry configuration
474+
cefor = 0.0225, -- kg / sec - fuel consumption for a single engine in afterburner configuration
473475
dpdh_m = 1800, -- altitude coefficient for max thrust -- altitude effects to thrust -- The best recommendation at this point is to start with these values between 2000 and 3000 and adjust as needed after initial flight testing
474476
dpdh_f = 1800, -- altitude coefficient for AB thrust ???? or altitude effects to fuel rate -- The best recommendation at this point is to start with these values between 2000 and 3000 and adjust as needed after initial flight testing
475477
table_data = {
@@ -723,8 +725,8 @@ A_29B = {
723725
mapclasskey = "P0091000024",
724726

725727
Guns = {
726-
MG_20({muzzle_pos = {0.96,-0.68, 2.32},_connector = "Point_Gun_01_R",rates = {1025},effect_arg_number = 350,mixes = {{1,2,2,3,3}},azimuth_initial = 0.0,elevation_initial = 1,supply_position = {4.5,0.22, 0.3}}),-- MITRAIL AVR 1
727-
MG_20({muzzle_pos = {0.96, -0.68, -2.32},_connector = "Point_Gun_01_L",rates = {1025},effect_arg_number = 436,mixes = {{1,2,2,3,3}},azimuth_initial = 0.0,elevation_initial = 1,supply_position = {2.0, -0.25, 0.8}}),-- MITRAIL AVR 2 B
728+
MG_20({muzzle_pos = {0.96,-0.68, 2.32},_connector = "Point_Gun_01_R",rates = {1025},effect_arg_number = 350,mixes = {{1,2,2,3,3}},azimuth_initial = 0.0,elevation_initial = 0,supply_position = {4.5,0.22, 0.3}}),-- MITRAIL AVR 1
729+
MG_20({muzzle_pos = {0.96, -0.68, -2.32},_connector = "Point_Gun_01_L",rates = {1025},effect_arg_number = 436,mixes = {{1,2,2,3,3}},azimuth_initial = 0.0,elevation_initial = 0,supply_position = {2.0, -0.25, 0.8}}),-- MITRAIL AVR 2 B
728730
},
729731
}
730732

‎Cockpit/Scripts/CMFD/CMFD_SMS_ID_defs.lua‎

Lines changed: 56 additions & 0 deletions
Original file line numberDiff line numberDiff line change
@@ -11,6 +11,9 @@ SMS_MODE_IDS = {
1111
AA = counter(),
1212
SJ = counter(),
1313
EJ = counter(),
14+
OTHER = counter(),
15+
CD = counter(),
16+
1417
}
1518

1619
count = -1
@@ -26,3 +29,56 @@ SMS_SUBFORM_IDS = {
2629
}
2730

2831

32+
count = -1
33+
SMS_FUSE_SEL_IDS = {
34+
NT = counter(),
35+
N = counter(),
36+
T = counter(),
37+
SAFE = counter(),
38+
}
39+
40+
count = -1
41+
SMS_LAUNCH_MODE_IDS = {
42+
CCIP = counter(),
43+
MAN = counter(),
44+
CCRP = counter(),
45+
DTOS = counter(),
46+
}
47+
48+
count = -1
49+
SMS_FUSE_TYPE_IDS = {
50+
IMPC = counter(),
51+
PROX = counter(),
52+
ONETIME = counter(),
53+
}
54+
55+
count = -1
56+
SMS_TIME_ALT_SEL_IDS = {
57+
AD = counter(),
58+
ADBA = counter(),
59+
FDBA = counter(),
60+
}
61+
62+
count = -1
63+
SMS_IS_UNIT_IDS = {
64+
M = counter (),
65+
MS = counter (),
66+
}
67+
68+
count = -1
69+
SMS_BR_RR_SEL_IDS = {
70+
BR = counter(),
71+
RR = counter(),
72+
}
73+
74+
75+
76+
count = -1
77+
SMS_PROF_SEL_IDS = {
78+
PROF1 = counter(),
79+
PROF2 = counter(),
80+
PROF3 = counter(),
81+
PROF4 = counter(),
82+
PROF5 = counter(),
83+
}
84+

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