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entry.lua
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entry.lua
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local self_ID = "F-16 High Fidelity Flight Dynamics Model"
declare_plugin(self_ID,
{
installed = true, -- if false that will be place holder , or advertising
dirName = current_mod_path,
version = "1.2.14-150110",
state = "installed",
info = _("F-16 Technology Demonstration. High Fidelity Flight Dynamics Model"),
binaries = { 'F16DemoFM', }, -- The DLL of the external flight model
--binaries = { 'F16DemoFM', 'F16ACockpit.dll', }, -- EFM + cockpit?
Skins =
{
{
--for simulator loading window etc.
name = "F-16Demo",
dir = "Theme"
},
},
Missions =
{
{
name = _("F-16Demo"),
dir = "Missions",
CLSID = "{CLSID5456456346CLSID}",
},
},
LogBook =
{
{
name = _("F-16Demo"),
type = "F-16Demo",
},
},
InputProfiles =
{
["F-16Demo"] = current_mod_path .. '/Input',
},
})
-- /declare_plugin()
---------------------------------------------------------------------------------------
--mounting 3d model paths and texture paths
mount_vfs_model_path (current_mod_path.."/Shapes")
mount_vfs_model_path (current_mod_path.."/Cockpit/Shapes")
mount_vfs_texture_path (current_mod_path.."/Cockpit/Textures")
mount_vfs_texture_path (current_mod_path.."/Textures/Avionics")
mount_vfs_texture_path (current_mod_path.."/Textures/Base_Textures")
mount_vfs_texture_path (current_mod_path.."/Textures/147thFW")
mount_vfs_texture_path (current_mod_path.."/Textures/Blue_Digital")
mount_vfs_texture_path (current_mod_path.."/Textures/Digital")
mount_vfs_liveries_path (current_mod_path.."/Liveries")
---------------------------------------------------------------------------------------
-- currently needed for DCS to detect plugin as flyable..
dofile(current_mod_path..'/Database/F16Demo.lua')
suspension =
{
{
mass = 200,
pos = {3.133, -1.6, 0},
moment_of_inertia = {1000,1000,1000},
damage_element = 83,
-- (deg?) Speed threshold of jamming during impact of rotation limiter
damage_omega = 30.0,
-- (deg?) Designed angle of retracted gear with horizontal axis
state_angle_0 = 6.131341662,
-- (deg?) Designed angle of extended gear with verrtical axis
state_angle_1 = -2.995164152,
-- (m) attachment point to fuselage along x-axis
mount_pivot_x = -0.274,
-- (m) attachment point to fuselage along y axis
mount_pivot_y = -0.118,
-- (m) distance from strut-axis to attachment point of piston to gear stand
mount_post_radius = 0.657,
-- (m) length of angle brace in retracted position
mount_length = 0.604555117,
-- (deg?) length of position vector from attachment point
mount_angle_1 = -3.138548523,
-- (m) distance from rotation-axis of strut to wheel-axis
post_length = 1.748,
-- (m) displacement of wheel relative to strut
wheel_axle_offset = 0.05,
-- Gear is self oriented
self_attitude = true,
yaw_limit = math.rad(89.0),
damper_coeff = 30.0,
amortizer_min_length = 0.0,
amortizer_max_length = 0.397,
amortizer_basic_length = 0.397,
amortizer_spring_force_factor = 1.6e+13,
amortizer_spring_force_factor_rate = 20.0,
amortizer_static_force = 80000.0,
amortizer_reduce_length = 0.377,
amortizer_direct_damper_force_factor = 45000.0,
amortizer_back_damper_force_factor = 15000.0,
wheel_radius = 0.479,
wheel_static_friction_factor = 0.65 , --Static friction when wheel is not moving (fully braked)
wheel_side_friction_factor = 0.65 ,
wheel_roll_friction_factor = 0.025, --Rolling friction factor when wheel moving
wheel_glide_friction_factor = 0.28 , --Sliding aircraft
wheel_damage_force_factor = 250.0, -- Tire is explosing due to hard landing
wheel_damage_speed = 150.0, -- Tire burst due to excessive speed
wheel_moment_of_inertia = 3.6, --wheel moi as rotation body
wheel_brake_moment_max = 15000.0, -- maximum value of braking moment , N*m
--[[
args_post = {0,3,5};
args_amortizer = {1,4,6};
args_wheel = {76,77,77};
args_wheel_yaw = {2,-1,-1};
--]]
arg_post = 0,
arg_amortizer = 1,
arg_wheel_rotation = 101,
arg_wheel_yaw = 2,
collision_shell_name = "WHEEL_F",
},
{
mass = 200,
pos = {-1.185, -1.603, -1.185},
moment_of_inertia = {1000,1000,1000},
damage_element = 83,
damage_omega = 30.0,
state_angle_0 = 6.131341662,
state_angle_1 = -2.995164152,
mount_pivot_x = -0.274,
mount_pivot_y = -0.118,
mount_post_radius = 0.657,
mount_length = 0.604555117,
mount_angle_1 = -3.138548523,
post_length = 1.748,
wheel_axle_offset = 0.05,
self_attitude = false,
yaw_limit = math.rad(89.0),
damper_coeff = 30.0,
amortizer_min_length = 0.0,
amortizer_max_length = 0.397,
amortizer_basic_length = 0.397,
amortizer_spring_force_factor = 1.6e+13,
amortizer_spring_force_factor_rate = 17.0,
amortizer_static_force = 25000.0,
amortizer_reduce_length = 0.377,
amortizer_direct_damper_force_factor = 55000.0,
amortizer_back_damper_force_factor = 10000.0,
wheel_radius = 0.68,
wheel_static_friction_factor = 0.65 ,
wheel_side_friction_factor = 0.65 ,
wheel_roll_friction_factor = 0.025,
wheel_glide_friction_factor = 0.28 ,
wheel_damage_force_factor = 650.0,
wheel_damage_speed = 150.0,
wheel_moment_of_inertia = 3.6, --wheel moi as rotation body
wheel_brake_moment_max = 15000.0, -- maximum value of braking moment , N*m
--[[
args_post = {0,3,5};
args_amortizer = {1,4,6};
args_wheel = {76,77,77};
args_wheel_yaw = {2,-1,-1};
--]]
arg_post = 3,
arg_amortizer = 4,
arg_wheel_rotation = 102,
arg_wheel_yaw = -1,
collision_shell_name = "WHEEL_L",
},
{
mass = 200,
pos = {-1.185, -1.603, 1.185},
moment_of_inertia = {1000,1000,1000},
damage_element = 83,
damage_omega = 30.0,
state_angle_0 = 6.131341662,
state_angle_1 = -2.995164152,
mount_pivot_x = -0.274,
mount_pivot_y = -0.118,
mount_post_radius = 0.657,
mount_length = 0.604555117,
mount_angle_1 = -3.138548523,
post_length = 1.748,
wheel_axle_offset = 0.05,
self_attitude = false,
yaw_limit = math.rad(89.0),
damper_coeff = 30.0,
amortizer_min_length = 0.0,
amortizer_max_length = 0.397,
amortizer_basic_length = 0.397,
amortizer_spring_force_factor = 1.6e+13,
amortizer_spring_force_factor_rate = 17.0,
amortizer_static_force = 25000.0,
amortizer_reduce_length = 0.377,
amortizer_direct_damper_force_factor = 55000.0,
amortizer_back_damper_force_factor = 10000.0,
wheel_radius = 0.68,
wheel_static_friction_factor = 0.65 ,
wheel_side_friction_factor = 0.65 ,
wheel_roll_friction_factor = 0.025,
wheel_glide_friction_factor = 0.28 ,
wheel_damage_force_factor = 650.0,
wheel_damage_speed = 150.0,
wheel_moment_of_inertia = 3.6, --wheel moi as rotation body
wheel_brake_moment_max = 15000.0, -- maximum value of braking moment , N*m
--[[
args_post = {0,3,5};
args_amortizer = {1,4,6};
args_wheel = {101,102,103};
args_wheel_yaw = {2,-1,-1};
--]]
arg_post = 5,
arg_amortizer = 6,
arg_wheel_rotation = 103,
arg_wheel_yaw = -1,
collision_shell_name = "WHEEL_R",
},
}
local FM =
{
[1] = self_ID,
[2] = "F16DemoFM", -- DLL binarires for FM
center_of_mass = { 0.183 , 0.261 , 0.0}, -- center of mass position relative to object 3d model center for empty aircraft
moment_of_inertia = {12874.0, 85552.1, 75673.6}, -- moment of inertia of empty aircraft
suspension = suspension, -- gear posts initialization
}
dofile(current_mod_path.."/Views.lua")
make_view_settings('F-16Demo', ViewSettings, SnapViews)
--make_flyable(obj_name,optional_cockpit path,optional_fm = {mod_of_fm_origin,dll_with_fm})
--make_flyable('F-16Demo', nil, FM, nil)
local support_cockpit = current_mod_path..'/Cockpit/'
make_flyable('F-16Demo', support_cockpit, FM, nil)
----------------------------------------------------------------------------------------
plugin_done()-- finish declaration , clear temporal data