diff Propellor/PropTestD6.pd @ 289:cf583cdc6d0c

Spokes patch added. Number of minor edits.
author Rod Selfridge <r.selfridge@qmul.ac.uk>
date Mon, 15 May 2017 08:01:35 +0100
parents 07fa2ffc27ab
children 6b6e66400537
line wrap: on
line diff
--- a/Propellor/PropTestD6.pd	Mon Apr 24 20:32:21 2017 +0100
+++ b/Propellor/PropTestD6.pd	Mon May 15 08:01:35 2017 +0100
@@ -4,7 +4,7 @@
 1;
 #X obj 405 79 s myMet;
 #X obj -251 527 hsl 70 15 0 5000 0 0 empty empty RPM 2 8 0 10 -262144
--1 -1 3036 1;
+-1 -1 1408 1;
 #X floatatom 147 583 5 0 0 0 - - -;
 #X obj 224 414 vu 15 120 empty empty -1 -8 0 10 -66577 -1 1 0;
 #X obj 287 414 vu 15 120 empty empty -1 -8 0 10 -66577 -1 1 0;
@@ -42,11 +42,11 @@
 -261682 -1 -66577 1634 1;
 #X obj 66 299 r GAIN;
 #X obj -278 417 hsl 70 15 0.1 3 0 0 empty empty Blade_Length 2 8 0
-10 -262144 -1 -1 2059 1;
+10 -262144 -1 -1 4663 1;
 #X floatatom -220 440 0 0 0 0 - - -;
 #X obj -281 376 loadbang;
 #X obj 78 497 hsl 100 20 0 2500 0 0 empty empty Throttle 2 10 0 10
--204800 -1 -1 8712 1;
+-204800 -1 -1 4039 1;
 #X text 117 583 RPM;
 #X floatatom 74 459 0 0 0 0 - - -;
 #X obj -268 685 hsl 70 15 2 4 0 0 empty empty Blades 2 8 0 10 -262144
@@ -58,7 +58,7 @@
 10 -203904 -1 -1 5601 1;
 #X floatatom 695 443 0 0 0 0 - - -;
 #X obj 456 425 hsl 70 15 0 5000 0 0 empty empty Horse_Power 2 8 0 10
--262144 -1 -1 414 1;
+-262144 -1 -1 5520 1;
 #N canvas 345 218 373 219 dist 0;
 #X obj -154 38 *~;
 #X obj -98 40 *~;
@@ -237,11 +237,11 @@
 #X connect 42 0 1 0;
 #X restore 349 362 pd startUp;
 #X obj 444 249 hsl 100 20 -5000 5000 0 0 empty empty PropX 6 10 0 10
--228856 -1 -1 5823 1;
+-228856 -1 -1 5445 1;
 #X obj 553 247 hsl 100 20 -5000 5000 0 0 empty empty PropY 6 10 0 10
--228856 -1 -1 4599 1;
+-228856 -1 -1 6435 1;
 #X obj 395 144 vsl 20 100 0 1500 0 0 empty empty PropZ 0 -9 0 10 -228856
--1 -1 533 1;
+-1 -1 5280 1;
 #X floatatom 486 282 0 0 0 0 - - -;
 #X floatatom 597 273 0 0 0 0 - - -;
 #X floatatom 399 254 0 0 0 0 - - -;
@@ -275,7 +275,7 @@
 #X text 240 576 Calculate the Azimuth and Elevation between the observer
 \, at the centre of coordinate system and point between propellors.
 Azimuth and elevation of the plane also calculated in.;
-#N canvas 216 304 656 584 centrePan 0;
+#N canvas 475 191 656 584 centrePan 0;
 #X obj 28 111 /~;
 #X obj 44 91 inlet~;
 #X obj 28 71 r~ PropX;
@@ -356,6 +356,7 @@
 #X connect 18 1 31 0;
 #X connect 19 0 20 0;
 #X connect 20 0 21 0;
+#X connect 20 0 33 0;
 #X connect 22 0 23 0;
 #X connect 23 0 18 0;
 #X connect 24 0 25 0;
@@ -373,7 +374,6 @@
 #X connect 34 0 42 0;
 #X connect 35 0 36 0;
 #X connect 36 0 37 0;
-#X connect 36 0 33 0;
 #X connect 38 0 22 0;
 #X connect 41 0 42 0;
 #X connect 42 0 43 0;
@@ -832,7 +832,7 @@
 #X connect 50 0 51 0;
 #X restore 284 102 pd Angles2;
 #X obj 593 137 hsl 80 20 0 360 0 0 empty empty Yaw(Azimuth) 2 10 0
-10 -232576 -1 -1 7002 1;
+10 -232576 -1 -1 1975 1;
 #X obj 809 137 hsl 80 20 -180 180 0 0 empty empty Roll 2 10 0 10 -232576
 -1 -1 3950 1;
 #X floatatom 863 165 0 0 0 0 - - -;
@@ -1076,12 +1076,12 @@
 #X text 255 664 Preset Flight Paths;
 #X text 267 596 Aircraft Selector;
 #X obj 812 37 hsl 80 20 -90 90 0 0 empty empty Pitch(Elevation) 2 10
-0 10 -232576 -1 -1 4296 1;
+0 10 -232576 -1 -1 3950 1;
 #X floatatom 829 83 0 0 0 0 - - -;
 #X obj 381 531 hsl 70 15 3.6 360 1 0 empty empty Yaw 2 8 0 10 -203904
--1 -1 6719 1;
+-1 -1 4823 1;
 #X obj 381 561 hsl 70 15 -90 90 0 0 empty empty Pitch 2 8 0 10 -204786
--1 -1 3752 1;
+-1 -1 3450 1;
 #X floatatom 457 530 0 0 0 0 - - -;
 #X floatatom 458 559 0 0 0 0 - - -;
 #X obj -25 636 r length;
@@ -1268,13 +1268,13 @@
 #X connect 45 0 26 0;
 #X connect 45 0 16 0;
 #X restore 693 699 pd pathSelector;
-#N canvas 107 381 1318 700 PropAnglesHQ 0;
+#N canvas 97 42 1318 700 PropAnglesHQ 0;
 #X obj 256 504 pack;
 #X obj 304 503 pack;
 #X obj 922 118 hsl 128 15 -5000 5000 0 0 empty empty x -2 -8 0 10 -262144
--1 -1 7470 1;
+-1 -1 6985 1;
 #X obj 913 160 hsl 128 15 -5000 5000 0 0 empty empty y -2 -8 0 10 -262144
--1 -1 5900 1;
+-1 -1 8255 1;
 #X obj 23 592 <;
 #X floatatom 22 616 0 0 0 0 - - -;
 #X obj 56 592 <;