/
ships.lua
1049 lines (954 loc) · 30.1 KB
/
ships.lua
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print("REMEMBER TO PORT ship6model!!!");
define_model('missile', {
info = {
bounding_radius = 4,
materials={ 'body' },
tags = {'ship'},
ship_defs = {
{
name = 'MISSILE_UNGUIDED',
forward_thrust = -4e5,
hull_mass=1,
price=100
}, {
name = 'MISSILE_GUIDED',
forward_thrust = -2e5,
reverse_thrust = 1e5,
angular_thrust = 2e4,
hull_mass=1,
price=100
}, {
name = 'MISSILE_SMART',
forward_thrust = -3e5,
reverse_thrust = 1.5e5,
angular_thrust = 2e4,
hull_mass=1,
price=100
}, {
name = 'MISSILE_NAVAL',
forward_thrust = -4e5,
reverse_thrust = 2e5,
angular_thrust = 2e4,
hull_mass=1,
price=100
}
},
},
static = function(lod)
set_material('body', 1,1,1,1)
use_material('body')
cylinder(8, v(0,0,1), v(0,0,-3), v(0,1,0), .25)
thruster(v(0,0,1), v(0,0,1), 10, true)
end
})
define_model('nosewheel', {
info = {
lod_pixels={5,50,0},
bounding_radius = 7,
materials={'leg','tyre'}
},
static = function(lod)
set_material('leg', .5, .5, .5, 1, .5, .5, .5, 2.0, 0, 0, 0)
set_material('tyre', .3, .3, .3, 1, 0,0,0, 1, 0, 0, 0)
use_material('leg')
local v6 = v(0, 0, 0)
local v7 = v(0, 3, 0)
local v8 = v(0, 5, 0)
local divs = lod*4
cylinder(divs, v6, v8, v(0,0,1), .4)
cylinder(divs, v7, v8, v(0,0,1), .5)
use_material('tyre')
xref_cylinder(divs, v(.5,5,0), v(1,5,0), v(0,0,1), 1.0)
end
})
define_model('nosewheelunit', {
info = {
bounding_radius = 7,
materials={'inside', 'matvar2'}
},
static = function(lod)
set_material('inside', .2,.2,.2,1, 0,0,0, 1, 0,0,0)
end,
dynamic = function(lod)
-- flaps
local v6 = v(1.5, 0, 6)
local v7 = v(1.5, 0, -1)
local v8 = v(0, 0, 6)
local v9 = v(0, 0, -1)
set_material('matvar2', get_arg_material(2))
use_material('inside')
zbias(1, v(0,0,0), v(0,1,0))
-- flap internal
xref_quad(v8, v6, v7, v9)
-- SHould use parameter material(2) here but param materials not done yet
use_material('matvar2')
local flap_ang = 0.5*math.pi*math.clamp(3*get_arg(0),0,1)
local wheel_ang = 0.5*math.pi*math.clamp(1.5*(get_arg(0)-0.34), 0, 1)
local vrot = 1.5*v(-math.cos(flap_ang), math.sin(flap_ang), 0)
xref_quad(v7, v6, v6+vrot, v7+vrot)
xref_quad(v7, v7+vrot, v6+vrot, v6)
call_model('nosewheel', v(0,0,0), v(1,0,0),
v(0,math.sin(wheel_ang),math.cos(wheel_ang)), 1.0)
zbias(0)
end
})
define_model('mainwheel', {
info = {
lod_pixels = {5,50,0},
bounding_radius = 8,
materials = {'leg', 'tyre'}
},
static = function(lod)
local v6 = v(0,0,0)
local v7 = v(0,3,0)
local v8 = v(0,5,0)
-- crossbar
local v13 = v(0, 5, 1.4)
local v14 = v(0, 5, -1.4)
local divs = 4*lod
set_material('leg', .5,.5,.5,1, 1,1,1, 2, 0,0,0)
use_material('leg')
cylinder(divs, v6, v8, v(0,0,1), .4)
cylinder(divs, v7, v8, v(0,0,1), .5)
cylinder(4, v13, v14, v(1,0,0), .5)
set_material('tyre', .3,.3,.3,1, 0,0,0, 1, 0,0,0)
use_material('tyre')
xref_cylinder(divs, v(.5, 5, 1.1), v(1, 5, 1.1), v(0,0,1), 1)
xref_cylinder(divs, v(.5, 5, -1.1), v(1, 5, -1.1), v(0,0,1), 1)
end
})
define_model('mainwheelunit', {
info = {
bounding_radius = 7,
materials={'inside','matvar2'}
},
static = function(lod)
set_material('inside', .2,.2,.2,1, 0,0,0, 1, 0,0,0)
end,
dynamic = function(lod)
-- flaps
local v6 = v(1.5, 0, 6)
local v7 = v(1.5, 0, -1)
local v8 = v(0, 0, 6)
local v9 = v(0, 0, -1)
set_material('matvar2', get_arg_material(2))
use_material('inside')
zbias(1, v(0,0,0), v(0,1,0))
-- flap internal
xref_quad(v8, v6, v7, v9)
-- SHould use parameter material(2) here but param materials not done yet
use_material('matvar2')
local flap_ang = 0.5*math.pi*math.clamp(3*get_arg(0),0,1)
local wheel_ang = 0.5*math.pi*math.clamp(1.5*(get_arg(0)-0.34), 0, 1)
local vrot = 1.5*v(-math.cos(flap_ang), math.sin(flap_ang), 0)
xref_quad(v7, v6, v6+vrot, v7+vrot)
xref_quad(v7, v7+vrot, v6+vrot, v6)
call_model('mainwheel', v(0,0,0), v(1,0,0),
v(0,math.sin(wheel_ang),math.cos(wheel_ang)), 1.0)
zbias(0)
end
})
define_model('ladybird', {
info = {
scale = 1,
lod_pixels = {50,100,200,0},
bounding_radius = 26, --35
materials={'white','engines','matvar0', 'matvar2',
'engine_inside','text'},
tags = {'ship'},
ship_defs = {
{
name='Ladybird Starfighter',
forward_thrust = -10e6,
reverse_thrust = 4e6,
up_thrust = 3e6,
down_thrust = -3e6,
left_thrust = -2e6,
right_thrust = 2e6,
angular_thrust = 4e6,
gun_mounts = { { v(0,-0.5,0), v(0,0,-1) }, { v(0,0,0), v(0,0,1) }, },
max_cargo = 60,
max_missile = 2,
max_laser = 2,
capacity = 60,
hull_mass = 60,
price = 87000,
hyperdrive_class = 1,
}
},
},
static = function(lod)
local v06 = v(-4.0, -5.0, -20.0);
local v07 = v(4.0, -5.0, -20.0);
local v08 = v(-6.0, 4.0, -10.0);
local v09 = v(6.0, 4.0, -10.0);
local v10 = v(-14.0, -5.0, -10.0);
local v11 = v(-10.0, 5.0, 10.0);
local v29 = v(10.0, 5.0, 10.0);
local v30 = v(14.0, -5.0, -10.0);
local v31 = v(-10.0, -5.0, 10.0);
local v32 = v(10.0, -5.0, 10.0);
local v33 = v(-12.0, 0.0, 10.0);
local v34 = v(-12.0, 0.0, 13.0);
--// thruster jets
local v38 = v(-12.0, 0.0, 13.0);
local v39 = v(-15.0, -3.0, -9.0);
local v40 = v(-30.0, -4.0, 9.0);
local v41 = v(-29.0, -5.5, 9.0);
local v42 = v(-29.0, -4.0, 9.0);
local v43 = v(-10.0, 0.0, -11.0);
xref_thruster(v38, v(0,0,1), 50, true)
xref_thruster(v43, v(0,0,-1), 25)
set_material('white',.5,.5,.5,1,1,1,1,100)
use_material('matvar0')
-- matvar(0)
if lod<2 then
texture('ships/default_ship_textures/lbfront_s.png', v(.5,.445,0), v(.085,0,0), v(0,.111,0))
else
texture('ships/default_ship_textures/lbfront_l.png', v(.5,.445,0), v(.085,0,0), v(0,.111,0))
end
quad(v06,v08,v09,v07)
if lod<2 then
texture('ships/default_ship_textures/lbtop_s.png', v(.5,.5,0), v(.05,0,0), v(0,0,1))
else
texture('ships/default_ship_textures/lbtop_l.png', v(.5,.5,0), v(.05,0,0), v(0,0,1))
end
quad(v09,v08,v11,v29)
if lod <2 then
texture('ships/default_ship_textures/lbside_s.png', v(1,.5,0), v(0,0,1), v(0,.1,0))
else
texture('ships/default_ship_textures/lbside_l.png', v(1,.5,0), v(0,0,1), v(0,.1,0))
end
xref_tri(v08,v06,v10)
local divs = lod*2
local wingtip_rear = v(30,-5,10)
local cpoint_rear = v(20,4,10)
local leadingedge_mid = v(24,-5,-3)
local tmp = v(5,0,5)
local cpoint_leadingedge1 = leadingedge_mid - tmp
local cpoint_leadingedge2 = leadingedge_mid + tmp
-- body flat side piece
if lod <2 then
texture('ships/default_ship_textures/lbside_s.png', v(.5,.5,0), v(0,0,.5), v(0,.1,0))
else
texture('ships/default_ship_textures/lbside_l.png', v(.5,.5,0), v(0,0,.5), v(0,.1,0))
end
local normal = ((v29-v09):cross(v30-v09)):norm()
local cpoint_bodycurve = 0.5*(v29+v30) + 3.0*(v29-v30):cross(normal):norm()
xref_flat(divs, normal,
{ v09 },
{ v29 },
{ cpoint_bodycurve, v30 }
)
-- top wing bulge
if lod<2 then
texture('ships/default_ship_textures/lbwing_s.png', v(.5,.5,0), v(.8,0,0), v(0,0,.8))
else
texture('ships/default_ship_textures/lbwing_s.png', v(.5,.5,0), v(.8,0,0), v(0,0,.8))
end
xref_quadric_bezier_quad(divs,divs,
wingtip_rear, cpoint_leadingedge2, leadingedge_mid,
cpoint_rear, v(17,5,0), cpoint_leadingedge1,
v29, cpoint_bodycurve, v30)
-- rear
if lod<2 then
texture('ships/default_ship_textures/lbrear_s.png', v(.5,.5,0), v(.017,0,0), v(0,.017,0))
else
texture('ships/default_ship_textures/lbrear_l.png', v(.5,.5,0), v(.017,0,0), v(0,.017,0))
end
xref_flat(divs, v(0,0,1),
{ wingtip_rear },
{ cpoint_rear, v29 },
{ v32 }
)
quad(v29,v11,v31,v32)
use_material('matvar2')
if lod<2 then
texture('ships/default_ship_textures/lbrear_s.png', v(.5,.4,0), v(.0165,0,0), v(0,0,1.2))
else
texture('ships/default_ship_textures/lbrear_l.png', v(.5,.4,0), v(.0165,0,0), v(0,0,1.2))
end
quad(v10,v06,v07,v30)
if lod<2 then
texture('ships/default_ship_textures/lbrear_s.png', v(.5,.8,0), v(.0165,0,0), v(0,0,1.2))
else
texture('ships/default_ship_textures/lbrear_l.png', v(.5,.8,0), v(.0165,0,0), v(0,0,1.2))
end
quad(v32,v31,v10,v30)
-- underside of wing
xref_tri(v30, wingtip_rear, v32)
-- wing leading edge underside
if lod<2 then
texture('ships/default_ship_textures/lbrear_s.png', v(.5,.31,0), v(.0165,0,0), v(0,0,.6))
else
texture('ships/default_ship_textures/lbrear_l.png', v(.5,.31,0), v(.0165,0,0), v(0,0,.6))
end
xref_flat(divs, v(0,-1,0),
{ v30 },
{ cpoint_leadingedge1, leadingedge_mid },
{ cpoint_leadingedge2, wingtip_rear }
)
if lod<2 then
texture('ships/default_ship_textures/lbwing_s.png', v(.5,.5,0), v(.1,0,0), v(0,0,15))
else
texture('ships/default_ship_textures/lbwing_l.png', v(.5,.5,0), v(.1,0,0), v(0,0,15))
end
zbias(1, v33, v(0,0,1))
set_material('engines',.3,.3,.3,1,.3,.3,.3,20)
use_material('engines')
xref_tube(4*lod, v33, v34, v(0,1,0), 2.5, 3.0)
use_material('engine_inside')
-- matanim!!
xref_circle(4*lod, v33, v(0,0,1), v(0,1,0), 2.5)
-- wheels my friend
end,
dynamic = function(lod)
set_material('matvar0', get_arg_material(0))
set_material('matvar2', get_arg_material(2))
set_material('engine_inside', lerp_materials(get_arg(2)*30.0, {0, 0, 0, 1, 0, 0, 0, 10, .5, .5, 1 },
{0, 0, 0, 1, 0, 0, 0, 10, 0, 0, .5 }))
set_material('text', 0,0,0,1,0.3,0.3,0.3,5)
if lod >0 then
use_material('text')
local label = get_arg_string(0)
zbias(1,v(8.9,3.6,.07),v(1.8,1,1))
text(label,v(8.9,3.6,.07),v(1.8,1,1),v(-.25,0,-1),1.5, {center=true})
zbias(1,v(-8.9,3.6,.07),v(1.8,1,1))
text(label,v(-8.9,3.6,.07),v(-1.8,1,1),v(-.25,0,1),1.5, {center=true})
zbias(0)
end
if get_arg(0) ~= 0 then
local v35 = v(0.0, -5.0, -13.0);
local v36 = v(-15.0, -5.0, 3.0);
local v37 = v(15.0, -5.0, 3.0);
zbias(1, v35, v(0,-1,0))
call_model('nosewheelunit', v35, v(-1,0,0), v(0,-1,0), 1)
call_model('mainwheelunit', v36, v(-1,0,0), v(0,-1,0), 1)
call_model('mainwheelunit', v37, v(-1,0,0), v(0,-1,0), 1)
zbias(0)
end
end
})
define_model('__walruswing', {
info = {
lod_pixels = { 20, 50, 0 },
scale = 25,
bounding_radius = 2.0,
materials = {'matvar0'}
},
static = function(lod)
-- bottom front
local v06 = v(0.0, 0.0, 1.0)
-- bottom back
local v07 = v(0.0, 0.0, -1.0)
-- top front
local v08 = v(0.0, 1.5, 0.0)
-- top back
local v09 = v(0.0, 1.5, -1.5)
use_material('matvar0')
local bend = v(0.175,0,0)
xref_quadric_bezier_quad(1,lod*4, v07, 0.5*(v07+v09), v09,
0.5*(v06+v07)+bend, bend, 0.5*(v08+v09)+bend,
v06, 0.5*(v06+v08), v08)
flat(lod*4, v(0,1,0), { 0.5*(v08+v09)+bend, v09 },
{ 0.5*(v08+v09)-bend, v08 })
end,
dynamic = function(lod)
set_material('matvar0', get_arg_material(0))
end
})
define_model('walrus', {
info = {
scale = 1.0,
bounding_radius = 70,
materials = {'matvar0', 'text'},
tags = { 'ship' },
ship_defs = {
{
name='Walrus',
forward_thrust = -40e6,
reverse_thrust = 12e6,
up_thrust = 10e6,
down_thrust = -6e6,
left_thrust = -6e6,
right_thrust = 6e6,
angular_thrust = 12e6,
gun_mounts = { { v(0,-0.5,0), v(0,0,-1) }, { v(0,0,0), v(0,0,1) }, },
max_cargo = 320,
max_laser = 2,
max_missile = 6,
capacity = 320,
hull_mass = 300,
price = 350000,
hyperdrive_class = 5,
}
}
},
static = function()
local v06 = v(-5.0, 10.0, -30.0)
-- 6, top four body verts
local v07 = v(5.0, 10.0, -30.0)
local v08 = v(-5.0, 10.0, 30.0)
local v09 = v(5.0, 10.0, 30.0)
local v10 = v(-11.16025, -0.6698729, -25.0)
-- 10, right four body verts
local v11 = v(-6.160254, -9.330127, -35.0)
local v12 = v(-11.16025, -0.6698729, 35.0)
local v13 = v(-6.160254, -9.330127, 30.0)
local v14 = v(11.16025, -0.6698729, -25.0)
-- 14, left four body verts
local v15 = v(6.160254, -9.330127, -35.0)
local v16 = v(11.16025, -0.6698729, 35.0)
local v17 = v(6.160254, -9.330127, 30.0)
local v18 = v(-5.0, -0.6698729, -60.0)
-- 18, front two verts
local v19 = v(5.0, -0.6698729, -60.0)
-- 20, top wing
local v20 = v(0.0, 10.0, 0.0)
local v21 = v(-1.0, 0.0, 0.0)
local v22 = v(0.0, 1.0, 0.0)
-- 23, right wing
local v24 = v(0.5, -0.8660254, 0.0)
local v25 = v(-0.8660254, -0.5, 0.0)
-- 26, left wing
local v27 = v(0.5, 0.8660254, 0.0)
local v28 = v(0.8660254, -0.5, 0.0)
local v29 = v(-0.0, 0.0, 40.0)
-- 29, main thruster
local v30 = v(-11.0, 0.0, -35.0)
-- 30, retro
local v31 = v(11.0, 0.0, -35.0)
local v32 = v(-9.0, 5.0, -30.0)
-- 32, right
local v33 = v(-12.0, -5.0, 30.0)
local v34 = v(12.0, -5.0, -30.0)
-- 34, left
local v35 = v(9.0, 5.0, 30.0)
local v36 = v(0.0, 12.0, -30.0)
-- 36, top
local v37 = v(0.0, 12.0, 30.0)
local v38 = v(0.0, -12.0, -30.0)
-- 38, bottom
local v39 = v(0.0, -12.0, 30.0)
local v42 = v(-5.0, 10.0, -30.0)
-- 6, top four body verts
local v43 = v(-11.16025, -0.6698729, 35.0)
use_material('matvar0')
quad(v07, v06, v08, v09)
quad(v13, v11, v15, v17)
xref_quad(v08, v06, v10, v12)
xref_quad(v12, v10, v11, v13)
quad(v09, v08, v12, v16)
quad(v16, v12, v13, v17)
quad(v06, v07, v19, v18)
quad(v18, v19, v15, v11)
xref_tri(v06, v18, v10)
xref_tri(v10, v18, v11)
thruster(v29, v(0,0,1), 50, true)
thruster(v30, v(0,0,-1), 35, true)
thruster(v31, v(0,0,-1), 35, true)
thruster(v32, v(-1,0,0), 25)
thruster(v33, v(-1,0,0), 25)
thruster(v34, v(1,0,0), 25)
thruster(v35, v(1,0,0), 25)
thruster(v36, v(0,1,0), 25)
thruster(v37, v(0,1,0), 25)
thruster(v38, v(0,-1,0), 25)
thruster(v39, v(0,-1,0), 25)
call_model('__walruswing', v20, v(-1,0,0), v(0,1,0), 1.0)
end,
dynamic = function(lod)
local v06 = v(-5.0, 10.0, -30.0)
local v07 = v(5.0, 10.0, -30.0)
local v08 = v(-5.0, 10.0, 30.0)
local v10 = v(-11.16025, -0.6698729, -25.0)
local v12 = v(-11.16025, -0.6698729, 35.0)
local v14 = v(11.16025, -0.6698729, -25.0)
local v16 = v(11.16025, -0.6698729, 35.0)
local v20 = v(0.0, 10.0, 0.0)
local v23 = v(-8.660254, -5.0, 0.0)
local v26 = v(8.660254, -5.0, 0.0)
local v40 = v(0.0, -9.330127, -30.0)
-- 40, nosewheel
local v41 = v(0.0, -9.330127, 13.0)
-- 41, mainwheel
local v54 = (v07 - v14):cross(v16 - v14):norm()
local v55 = (v06 - v08):cross(v12 - v08):norm()
set_material('matvar0', get_arg_material(0))
set_material('text', .2,.2,.2,1)
use_material('text')
geomflag(0x8000)
local reg = get_arg_string(0)
zbias(1, v16, v54)
text(reg, v16, v54, v(0,0,-1), 10.0, {xoffset=1, yoffset=.3})
zbias(1, v10, v55)
text(reg, v10, v55, v(0,0,1), 10.0, {xoffset=.8, yoffset=.3})
geomflag(0)
if get_arg(0) > 0 then
zbias(1, v40, v(0,-1,0))
call_model('nosewheelunit', v40, v(-1,0,0), v(0,-1,0), 2.0)
call_model('mainwheelunit', v41, v(-1,0,0), v(0,-1,0), 2.0)
end
zbias(0)
local ang = math.pi - 0.5 + 0.5*get_arg(0)
local xaxis = v(math.sin(ang), math.cos(ang), 0)
call_model('__walruswing', v23, xaxis, v(0,0,-1):cross(xaxis), 1.0)
ang = 0.5 - 0.5*get_arg(0)
local xaxis = v(math.sin(ang), math.cos(ang), 0)
call_model('__walruswing', v26, xaxis, v(0,0,-1):cross(xaxis), 1.0)
end
})
define_model('flowerfairy', {
info = {
scale=2.0,
lod_pixels = {25,50,0},
bounding_radius = 100,
materials = {'matvar0','gray','text','engine_inside'},
tags = {'ship'},
ship_defs = {
{
name='Flowfairy Heavy Trader',
forward_thrust = -60e6,
reverse_thrust = 20e6,
up_thrust = 20e6,
down_thrust = -10e6,
left_thrust = -10e6,
right_thrust = 10e6,
angular_thrust = 20e6,
gun_mounts = { { v(0,-0.5,0), v(0,0,-1) }, { v(0,0,0), v(0,0,1) }, },
max_cargo = 500,
max_laser = 2,
max_missile = 4,
capacity = 500,
hull_mass = 500,
price = 550000,
hyperdrive_class = 6,
}
}
},
static = function(lod)
-- // 6, nose vertices
local v06 = v(4.0, -3.0, -35.0)
local v07 = v(-4.0, -3.0, -35.0)
local v08 = v(-1.0, -7.0, -32.0)
local v09 = v(1.0, -7.0, -32.0)
-- // 10, nose section back
local v10 = v(6.0, 8.0, -20.0)
local v11 = v(-6.0, 8.0, -20.0)
local v12 = v(-10.0, 4.0, -20.0)
local v13 = v(-10.0, -4.0, -20.0)
local v14 = v(-6.0, -8.0, -20.0)
local v15 = v(6.0, -8.0, -20.0)
local v16 = v(10.0, -4.0, -20.0)
local v17 = v(10.0, 4.0, -20.0)
-- midpoints
local v18 = v(0.0, 0.0, -20.0)
local v19 = v(0.0, 0.0, -16.0)
local v20 = v(0.0, 0.0, 4.0)
local v21 = v(0.0, 0.0, 8.0)
local v22 = v(0.0, 0.0, 26.0)
-- // 24, top engine
local v24 = v(-12.5, 2.0, 10.0)
local v25 = v(-12.5, 2.0, 30.0)
local v26 = v(-12.5, 2.0, 13.0)
local v27 = v(-12.5, 2.0, 27.0)
-- // 28, bottom engine
local v28 = v(-12.0, -5.5, 10.0)
local v29 = v(-12.0, -5.5, 30.0)
local v30 = v(-12.0, -5.5, 13.0)
local v31 = v(-12.0, -5.5, 27.0)
-- 41, extrusion as at 10 but rev order
local v41 = v(6.0, 8.0, -20.0)
local v42 = v(-6.0, 8.0, -20.0)
local v43 = v(-10.0, 4.0, -20.0)
local v44 = v(-10.0, -4.0, -20.0)
local v45 = v(-6.0, -8.0, -20.0)
local v46 = v(6.0, -8.0, -20.0)
local v47 = v(10.0, -4.0, -20.0)
local v48 = v(10.0, 4.0, -20.0)
set_material('text', .20, .20, .20, 1)
use_material('matvar0')
quad(v06,v07,v11,v10)
xref_tri(v07,v12,v11)
xref_tri(v07,v13,v12)
xref_tri(v07,v14,v13)
xref_tri(v07,v08,v14)
quad(v07,v06,v09,v08)
quad(v08,v09,v15,v14)
quad(v10,v11,v14,v15)
xref_quad(v11,v12,v13,v14)
extrusion(v19, v20, v(0,1,0), 1.0,
v41, v42, v43, v44, v45,v46,v47,v48)
extrusion(v21, v22, v(0,1,0), 1.0,
v41, v42, v43, v44, v45,v46,v47,v48)
xref_tube(8, v24, v25, v(0,1,0), 2.0, 2.5)
xref_tube(8, v28, v29, v(0,1,0), 2.0, 2.5)
use_material('engine_inside')
xref_circle(8, v26, v(0,0,-1), v(0,1,0), 2)
xref_circle(8, v27, v(0,0,1), v(0,1,0), 2)
xref_circle(8, v30, v(0,0,-1), v(0,1,0), 2)
xref_circle(8, v31, v(0,0,1), v(0,1,0), 2)
set_material('gray', .30, .30, .30,1, .10, .10, .10, 10)
use_material('gray')
extrusion(v18, v19, v(0,1,0), .85,
v41, v42, v43, v44, v45,v46,v47,v48)
extrusion(v20, v21, v(0,1,0), .85,
v41, v42, v43, v44, v45,v46,v47,v48)
xref_thruster(v25, v(0,0,1), 30, true)
xref_thruster(v29, v(0,0,1), 30, true)
xref_thruster(v24, v(0,0,-1), 20, true)
xref_thruster(v28, v(0,0,-1), 20, true)
end,
dynamic = function(lod)
set_material('matvar0', get_arg_material(0))
set_material('engine_inside', lerp_materials(get_arg(2)*30.0, {0, 0, 0, 1, 0, 0, 0, 10, .5, .5, 1 },
{0, 0, 0, 1, 0, 0, 0, 10, 0, 0, .5 }))
-- 34, gear pos
local v34 = v(-5.0, -8.0, -13.0)
local v35 = v(5.0, -8.0, -13.0)
local v36 = v(-11.5, -8.0, 25.0)
local v37 = v(11.5, -8.0, 25.0)
local v38 = v(-11.5, -8.0, 13.0)
local v39 = v(11.5, -8.0, 13.0)
-- 40, dish pos
local v40 = v(-0.05, 8.0, 15.0)
local leftText = v(-10.0, 0, -6.4)
local rightText = v(10.0, 0, -6.4)
local reg = get_arg_string(0)
-- this means ignore in collision mesh
geomflag(0x8000)
use_material('text')
zbias(1, leftText, v(-1,0,0))
text(reg, leftText, v(-1,0,0), v(0,0,1), 4, {center=true})
zbias(1, rightText, v(1,0,0))
text(reg, rightText, v(1,0,0), v(0,0,-1), 4, {center=true})
geomflag(0)
if get_arg(0) > 0 then
zbias(1, v34, v(0,-1,0))
call_model('mainwheelunit', v34, v(-1,0,0), v(0,-1,0), .6)
call_model('mainwheelunit', v35, v(-1,0,0), v(0,-1,0), .6)
call_model('mainwheelunit', v36, v(-1,0,0), v(0,-1,0), .5)
call_model('mainwheelunit', v37, v(-1,0,0), v(0,-1,0), .5)
call_model('mainwheelunit', v38, v(-1,0,0), v(0,-1,0), .5)
call_model('mainwheelunit', v39, v(-1,0,0), v(0,-1,0), .5)
end
--[[
PTYPE_ZBIAS, 40, 1, 1,
PTYPE_SUBOBJECT, 0x8000, SUB_DISH, 40, 1, 100, 200,
PTYPE_ZBIAS, 0x8000, 0, 0,
--]]
zbias(0)
end
})
define_model('interdictor', {
info = {
lod_pixels = { 50, 100, 200, 0 },
bounding_radius = 50,
materials = {'matvar0', 'matvar2', 'engine', 'engine_inside', 'cockpit', 'text'},
tags = {'ship'},
ship_defs = {
{
name='Sirius Interdictor',
forward_thrust = -24e6,
reverse_thrust = 12e6,
up_thrust = 6e6,
down_thrust = -6e6,
left_thrust = -6e6,
right_thrust = 6e6,
angular_thrust = 12e6,
gun_mounts = { { v(0,-0.5,0), v(0,0,-1) }, { v(0,-0.5,0), v(0,0,1) }, },
max_cargo = 90,
max_laser = 2,
max_missile = 8,
capacity = 90,
hull_mass = 100,
price = 160000,
hyperdrive_class = 4,
}
}
},
static = function(lod)
local nose_tip = v(0.0, 0.0, -35.0)
--f } }, // 6, nose point
local v07 = norm(0.0, 1.0, -0.2)
--} }, // nose normal
local front_lateral = v(-6.0, 0.0, -18.0)
--} }, // 8, r edge forward mid
local v09 = norm(-0.2, 1.0, -0.1)
--} }, // norm
local v10 = v(-12.0, 0.0, 2.0)
--} }, // 10, r edge back mid
local v11 = norm(-0.2, 1.0, -0.1)
--} }, // norm
local v12 = v(-7.5, 0.0, 25.0)
--} }, // 12, r edge back
local v13 = norm(0.0, 1.0, 0.2)
--} }, // norm
local v14 = v(0.0, 3.0, -15.0)
--} }, // 14, cockpit front
local v15 = norm(0.0, 1.0, 0.08)
--} }, // norm
local v16 = v(-1.5, 3.0, -13.5)
--} }, // 16, cockpit right
local v17 = norm(0.0, 1.0, 0.08)
--} }, // norm
local v18 = v(0.0, 3.0, -10.0)
--} }, // 18, cockpit back
local v19 = norm(0.0, 1.0, 0.08)
--} }, // norm
local v20 = v(1.5, 3.0, -13.5)
--} }, // 20, cockpit left
local v21 = norm(0.0, 1.0, 0.08)
--} }, // norm
local v22 = v(-6.0, 3.0, 5.0)
--} }, // 22, inner right
local v23 = norm(-0.2, 1.0, -0.2)
--} }, // norm
local v24 = v(0.0, 3.0, 5.0)
--} }, // 24, inner mid
local v25 = norm(0.2, 1.0, -0.2)
--} }, // norm
local v26 = v(-2.0, 2.0, -23.0)
--} }, // 26, fwd midpoint
local v27 = norm(0.0, 1.0, -0.1)
--} }, // norm
local v28 = v(-5.0, 2.5, -5.0)
--} }, // 28, right midpoint
local v29 = norm(-0.08, 1.0, -0.04)
--} }, // norm
local v30 = v(-7.0, 2.0, 14.0)
--} }, // 30, rear right midpoint
local v31 = norm(-0.04, 1.0, 0.1)
--} }, // norm
local v32 = v(-3.0, 3.0, -5.0)
--} }, // 32, central midpoint
local v33 = v(0.0, 4.0, -12.5)
--} }, // 33, cockpit midpoint
local v34 = v(-3.75, 4.0, 20.0)
--} }, // 34, nacelle midpoint
local v35 = v(-7.5, 0.0, 30.0)
--} }, // 35, nacelle outer
local v36 = v(0.0, 0.0, 30.0)
--} }, // 36, nacelle inner
-- edge tangents
local v37 = v(6.0, 4.0, 3.0)
--} }, // 37, edge to mid
local v38 = v(6.0, 0.0, 3.0)
local v39 = v(0.0, 4.0, -20.0)
--} }, // 39, rear to mid
local v40 = v(2.5, 0.0, -20.0)
local v41 = v(0.0, 0.0, -20.0)
--} }, // 41, mid to nose
local v42 = v(0.0, -4.0, -20.0)
local v43 = v(-6.0, 0.0, -3.0)
--} }, // 43, mid to edge
local v44 = v(-6.0, -4.0, -3.0)
local v45 = v(-2.5, 0.0, 20.0)
--} }, // 45, mid to rear
local v46 = v(0.0, -4.0, 20.0)
local v47 = v(-1.5, 0.0, 0.0)
--} }, // 47, cockpit CW tangents
local v48 = v(1.5, 0.0, 0.0)
local v49 = v(0.0, 0.0, -1.5)
local v50 = v(0.0, 0.0, 1.5)
local v51 = v(0.0, 0.0, -3.5)
local v52 = v(0.0, 0.0, 3.5)
local v53 = v(-10.0, 0.0, 20.0)
--} }, // 53, rear edge tangents
local v54 = v(10.0, 0.0, 0.0)
local v55 = v(4.0, 0.0, -10.0)
--} }, // 55, CCW
local v56 = v(-5.0, 0.0, -10.0)
local v57 = v(0.0, 1.5, 0.0)
--} }, // 57, nacelle tangents
local v58 = v(0.0, -1.5, 0.0)
local v59 = v(0.0, 0.0, -12.0)
local v60 = v(0.0, 0.0, 12.0)
local v61 = v(-3.75, 4.0, 30.0)
--} }, // 61, nacelle rear midpoint
local v62 = v(-3.0, 0.0, 0.0)
--} }, // and tangents
local v63 = v(4.0, 0.0, 0.0)
--} }, //
-- underside points
local v64 = v(-5.0, 0.0, -5.0)
--} }, // 64, upper outer vent
local v65 = v(0.0, 0.0, -5.0)
--} }, // 65, upper inner vent
local v66 = v(-5.0, -2.0, -3.0)
--} }, // 66, lower outer vent
local v67 = v(0.0, -2.0, -3.0)
--} }, // 67, lower inner vent
local v68 = v(-5.0, -2.0, 30.0)
--} }, // 68, nacelle outer underside
local v69 = v(0.0, -2.0, 30.0)
--} }, // 69, nacelle inner underside
local v70 = v(-13.0, 0.0, 14.0)
--} }, // 70, rear underside centre
local v71 = v(-7.5, 0.0, -3.0)
--} }, // 71, vent outer edge
local v72 = v(-3.75, 0.7, 30.0)
--} }, // 72, engine midpoint
local v76 = v(-3.75, 0.7, 32.0)
--} }, // 76, engine end
local v77 = v(-4.5, -0.3, -4.7)
--} }, // 77, retro vent
local v78 = v(-0.5, -0.3, -4.7)
local v79 = v(-4.5, -1.7, -3.3)
local v80 = v(-0.5, -1.7, -3.3)
use_material('matvar0')
local lvl = lod * 4
local c14_6_1 = vlerp(.75,nose_tip,v14)
local c16_8_1 = v(-2.5, 3.0, -13.5)
local j = v(-2,2.0,-21)
nose_patch = {nose_tip, vlerp(.25,nose_tip,front_lateral), vlerp(.75,nose_tip,front_lateral), front_lateral,
v(0.0,0.75,-30.0), v(-2,0.75,-30), v(-4,1.75,-21), v(-4.875,1.75,-16.875),
v(0.0,2.25,-20.0), v(-2,2.25,-20), v(-1.875,2.8125,-15.125), v(-2.5,3,-13.5),
v14,v(-0.375,3.0,-14.625),v(-1.125,3.0,-13.875),v16}
-- top nose bit
xref_cubic_bezier_quad(lvl, lvl, nose_patch)
local c22_10_1 = v(-10.0, 3.0, 4.0)
local c22_10_2 = v(-12.0, 1.0, 4.0)
-- side thingies
j = 0.25*(v10+v22+v16+front_lateral)
side_patch = joined_patch(nose_patch, 1, {
vlerp(.75, v16, v22), v(-9,3,0), v(-10,1,0.0), vlerp(.75,front_lateral,v10),
v22, c22_10_1, c22_10_2, v10 })
--local v10 = v(-12.0, 0.0, 2.0)
xref_cubic_bezier_quad(lvl, lvl, side_patch)
j = 0.333*(v12+v22+v10)+v(0,5,0)
local wingtip = v(-14.1, 0, 12)
top_wing_patch = joined_patch(side_patch, 2, {
vlerp(.75,v22,v12),v(-9,1,15),v(-11,2,12),wingtip-v(0,0,5),
v12, v12+v(-5,0,-6), wingtip+v(0,0,5), wingtip})
xref_cubic_bezier_quad(lvl, lvl, top_wing_patch)
-- top wings
local engine_back_cp1 = v(-1,5.4,0)
local engine_back_cp2 = v(1,5.4,0)
local c1_1 = v(0, 1.0, 25.0)
local j = 0.25*(c1_1 + v36 + v35 + v12)
local c2_1 = v(0, 3.0, 5.0)
-- front bit of top curve of engine
front_top_engine_patch = {c2_1, c2_1+v(-2,0,-4), v22+v(2,0,-4), top_wing_patch[1],
vlerp(.25,c2_1,c1_1), vlerp(.25,c2_1,c1_1)+v(0,1.5,0), vlerp(.25,v22,v12)+v(0,3,0), top_wing_patch[5],
vlerp(.75,c2_1,c1_1), vlerp(.75,c2_1,c1_1)+0.7*engine_back_cp1, vlerp(.75,v22,v12)+0.7*engine_back_cp2, top_wing_patch[9],
c1_1, c1_1+0.85*engine_back_cp1, v12+0.85*engine_back_cp2, top_wing_patch[13]}
xref_cubic_bezier_quad(lvl, lvl, front_top_engine_patch)
rear_top_engine_curve = joined_patch(front_top_engine_patch, 2, {
vlerp(0.75,c1_1,v36), vlerp(0.75,c1_1,v36)+engine_back_cp1, vlerp(0.75,v12,v35)+engine_back_cp2, vlerp(0.75,v12,v35),
v36, v36+v(-1,5.4,0), v35+v(1,5.4,0), v35})
xref_cubic_bezier_quad(1, lvl, rear_top_engine_curve)
-- flat bit where cockpit sits.
xref_flat(lvl, v(0,1,0),
{ v16 },
{ side_patch[5], side_patch[9], v22 },
{ v22+v(2,0,-4), c2_1+v(-2,0,-4), c2_1 },
{ v14 })
use_material('matvar2')
-- Underside of wings
xref_flat(lvl, v(0,-1,0),
{ top_wing_patch[14], top_wing_patch[15], top_wing_patch[16] },
{ top_wing_patch[12], top_wing_patch[8], top_wing_patch[4] },
{ v71 }, { v12 })
-- other underside
xref_quad(front_lateral,nose_tip,v65,v64)
xref_quad(front_lateral,v64,v71,v10)
xref_quad(v64,v65,v67,v66)
xref_tri(v71,v64,v66)
xref_quad(v71,v66,v68,v12)
xref_tri(v12,v68,v35)
xref_quad(v66,v67,v69,v68)
-- engine back face
xref_flat(lvl, v(0,0,1),
{ v36+engine_back_cp1, v35+engine_back_cp2, v35 },
{ v68 }, { v69 }, { v36 })
set_material('cockpit', .3,.3,.3,1, .3,.3,.3, 20)
use_material('cockpit')
quadric_bezier_quad(lvl, lvl,
v18, 0.5*(v18+v20)+v(1,0,0), v20,
0.5*(v16+v18)-v(1,0,0), v(0,6,-10), 0.5*(v20+v14),
v16, 0.5*(v14+v16),v14)
set_material('engine', .30, .30, .30,1, .30, .30, .30, 20)
use_material('engine')
xref_tube(lvl, v72, v76, v(0,1,0), 2.0, 2.5)
if lod > 1 then
zbias(1, v72, v(0,0,1))
use_material('engine_inside')
xref_circle(lvl, v72, v(0,0,1), v(0,1,0), 2.0)
local retro_norm = ((v80-v78):cross(v77-v78)):norm()
zbias(1, v77, retro_norm)
xref_quad(v77, v78, v80, v79)
zbias(0)
end
set_material('text', .2,.2,.2,1)
-- main & retro thrusters
local v82 = v(3.75, 0.7, 32.0)
local v84 = v(2.5, -1.0, -5.0)
-- vertical thrusters
local v85 = v(-9.0, 1.5, 10.0)
local v86 = v(-9.0, -0.5, 10.0)
local v87 = v(9.0, 1.5, 10.0)
local v88 = v(9.0, -0.5, 10.0)
local v89 = v(0.0, 3.5, -8.0)
local v90 = v(0.0, -0.5, -25.0)
-- horizontal thrusters
local v91 = v(-8.0, 0.0, 28.0)
local v92 = v(8.0, 0.0, 28.0)
local v93 = v(-3.5, 0.0, -25.0)
local v94 = v(3.5, 0.0, -25.0)
xref_thruster(v82, v(0,0,1), 30, true)
xref_thruster(v84, v(0,0,-1), 20, true)
thruster(v85, v(0,1,0), 15)
thruster(v86, v(0,-1,0), 15)
thruster(v87, v(0,1,0), 15)
thruster(v88, v(0,-1,0), 15)
thruster(v89, v(0,1,0), 15)
thruster(v90, v(0,-1,0), 15)
thruster(v91, v(-1,0,0), 15)
thruster(v92, v(1,0,0), 15)