Read time: 2.5 minutes (253 words)
Position CatalogΒΆ
Name |
Value |
File |
|---|---|---|
$fn |
||
100 |
fuselage/wing_post/wing_post.scad |
|
100 |
fuselage/stab_post/stab_post.scad |
|
arc_pos |
||
[tip_radius, -tip_span + tip_radius, 0,0,0,0] |
stab/left_tip/left_tip_pos.scad |
|
[fin_radius, -fin_span + fin_radius, 0,0,0,0] |
fuselage/fin/fin_pos.scad |
|
[tip_radius, -tip_span + tip_radius, 0,0,0,0] |
wing/left_tip/left_tip_pos.scad |
|
[tip_radius, -tip_span + tip_radius, 0,0,0,0] |
wing/left_tip/tip_arc/tip_arc_pos.scad |
|
center_pos |
||
[0,0,0,0,0,0] |
stab/stab_pos.scad |
|
[0,0,0,0,0,0] |
wing/wing_pos.scad |
|
covering_pos |
||
[0,-center_span/2,spar_size,0,0,0] |
stab/center/center_pos.scad |
|
[0,0,0,0,0,0] |
fuselage/fin/fin_pos.scad |
|
[0,-center_span/2,spar_size,0,0,0] |
wing/center/center_pos.scad |
|
fin_pos |
||
[xf,-xt,5/64,90,-tail_boom_angle,0] |
fuselage/fuselage_pos.scad |
|
fsp_pos |
||
[xfsp,ysp,0,0,0,0] |
fuselage/fuselage_pos.scad |
|
fuse_pos |
||
[0,0,0,0,0,0] |
math_magik_lpp_pos.scad |
|
fwp_pos |
||
[fp_offset,-ms_thickness/2-post_diameter/2,0,0,0,0] |
fuselage/fuselage_pos.scad |
|
le_pos |
||
[0,0,0,0,0,0] |
stab/center/center_pos.scad |
|
[0,0,0,0,0,-90] |
stab/left_tip/left_tip_pos.scad |
|
[0,-fin_le_length/2-spar_size,0,0,0,0] |
fuselage/fin/fin_pos.scad |
|
[0,0,0,0,0,0] |
wing/center/center_pos.scad |
|
[0,0,0,0,0,-90] |
wing/left_tip/left_tip_pos.scad |
|
left_tip_cover_pos |
||
[0,0,0,0,0,0] |
stab/left_tip/left_tip_pos.scad |
|
[0,0,0,0,0,0] |
wing/left_tip/left_tip_pos.scad |
|
left_tip_pos |
||
[0, -center_span/2, 0, 0,0,0] |
stab/stab_pos.scad |
|
[0, -center_span/2, 0, -tip_dihedral_angle,0,0] |
wing/wing_pos.scad |
|
ms_pos |
||
[0,ms_thickness/2,0,90,0,0] |
fuselage/fuselage_pos.scad |
|
pos_blade1 |
||
[0,0,prop_blade_offset,0,0,prop_pitch_angle] |
prop/prop_pos.scad |
|
pos_blade2 |
||
[0,0,-prop_blade_offset,180,0,-prop_pitch_angle] |
prop/prop_pos.scad |
|
pos_spar |
||
[0,0,0,0,0,0] |
prop/prop_pos.scad |
|
pos_wire_shaft |
||
[-1/64,0,0,0,0,0] |
prop/prop_pos.scad |
|
prop_pos |
||
[prop_x_offset, 0, prop_z_offset, -40,0,0] |
math_magik_lpp_pos.scad |
|
rh_pos |
||
[ms_length,0,0,0,0,0] |
fuselage/fuselage_pos.scad |
|
rib1_pos |
||
[spar_size,-center_span/2+spar_size/2,0,0,0,0] |
stab/center/center_pos.scad |
|
[tip_rib_chord/2 + tip_radius,-tip_span,0,0,0,90] |
stab/left_tip/left_tip_pos.scad |
|
[fin_chord/2,-spar_size,0,0,0,90] |
fuselage/fin/fin_pos.scad |
|
[spar_size,-center_span/2+spar_size/2,0,0,0,0] |
wing/center/center_pos.scad |
|
[tip_rib_chord/2 + tip_radius,-tip_span,0,0,0,90] |
wing/left_tip/left_tip_pos.scad |
|
rib2_pos |
||
[spar_size,0,0,0,0,0] |
stab/center/center_pos.scad |
|
[(fin_chord+fin_radius)/2-spar_size/2,-fin_span,0,0,0,90] |
fuselage/fin/fin_pos.scad |
|
[spar_size,-center_span/4,0,0,0,0] |
wing/center/center_pos.scad |
|
rib3_pos |
||
[spar_size,center_span/2-spar_size/2,0,0,0,0] |
stab/center/center_pos.scad |
|
[spar_size,0,0,0,0,0] |
wing/center/center_pos.scad |
|
rib4_pos |
||
[spar_size,center_span/4,0,0,0,0] |
wing/center/center_pos.scad |
|
rib5_pos |
||
[spar_size,center_span/2-spar_size/2,0,0,0,0] |
wing/center/center_pos.scad |
|
right_tip_pos |
||
[0, center_span/2, 0, 0,0,0] |
stab/stab_pos.scad |
|
[0, center_span/2, 0, tip_dihedral_angle,0,0] |
wing/wing_pos.scad |
|
rsp_pos |
||
[xrsp,ysp,0,0,0,0] |
fuselage/fuselage_pos.scad |
|
rwp_pos |
||
[rp_offset,-ms_thickness/2-post_diameter/2,0,0,0,0] |
fuselage/fuselage_pos.scad |
|
stab_le_mount_pos |
||
[-post_diameter/2-tube_thickness,0,0,0,0,0] |
stab/stab_pos.scad |
|
stab_pos |
||
[stab_x_offset,-stab_y_offset,stab_elevation,0,0,0] |
math_magik_lpp_pos.scad |
|
stab_te_mount_pos |
||
[max_stab_chord+post_diameter/2+tube_thickness,0,0,0,0,0] |
stab/stab_pos.scad |
|
stab_y_offset |
||
ms_thickness/2 + tb_thickness + post_diameter/2 |
math_magik_lpp_pos.scad |
|
t |
||
post_diamete |
fuselage/wing_post/wing_post.scad |
|
post_diamete |
fuselage/stab_post/stab_post.scad |
|
tb_pos |
||
[ms_length - 1/8, -ms_thickness/2-tb_thickness/2,0,0,0,0] |
fuselage/fuselage_pos.scad |
|
te_pos |
||
[max_stab_chord - spar_size,0,0,0,0,0] |
stab/center/center_pos.scad |
|
[max_stab_chord - spar_size,0,0,0,0,-90] |
stab/left_tip/left_tip_pos.scad |
|
[fin_chord - spar_size,-fin_te_length/2 - spar_size,0,0,0,0] |
fuselage/fin/fin_pos.scad |
|
[max_wing_chord - spar_size,0,0,0,0,0] |
wing/center/center_pos.scad |
|
[max_wing_chord - spar_size,0,0,0,0,-90] |
wing/left_tip/left_tip_pos.scad |
|
thb_pos |
||
[-thb_length+1/4,0,-thb_height,0,0,0] |
fuselage/fuselage_pos.scad |
|
wing_le_mount_pos |
||
[-post_diameter/2-tube_thickness,0,0,0,0,0] |
wing/wing_pos.scad |
|
wing_pos |
||
[wing_x_offset,-ms_thickness/2-post_diameter/2,wing_elevation,0,0,0] |
math_magik_lpp_pos.scad |
|
wing_te_mount_pos |
||
[max_wing_chord+post_diameter/2+tube_thickness,0,0,0,0,0] |
wing/wing_pos.scad |
|
xf |
||
ms_length + tail_boom_length - 1/8 - max_stab_chord |
fuselage/fuselage_pos.scad |
|
xfsp |
||
xf-post_diameter/2 |
fuselage/fuselage_pos.scad |
|
xrsp |
||
xf+max_stab_chord+post_diameter/2 |
fuselage/fuselage_pos.scad |
|
xt |
||
(ms_thickness + tb_thickness-thb_thickness)/2 |
fuselage/fuselage_pos.scad |
|
ysp |
||
-ms_thickness/2-tb_thickness-post_diameter/2 |
fuselage/fuselage_pos.scad |
|
z1 |
||
wing_post_height |
fuselage/wing_post/wing_post.scad |
|
stab_post_height |
fuselage/stab_post/stab_post.scad |
|
z2 |
||
wing_post_height-tube_height |
fuselage/wing_post/wing_post.scad |
|
stab_post_height-tube_height |
fuselage/stab_post/stab_post.scad |