"� > <BasicSave$dir>.KAM_ATRACT
�"Strange Attractors 1"
�"The KAM attractor"
(�"By Mike Cook"
22�"A defines the Angle of the orbit in radians"
<�
F0�"Enter a value for A about (1.1 to 1.7) ",A
P�0
Z,� �0,0);"The KAM attractor By Mike Cook"
d
sinA=�(A)
n
cosA=�(A)
xC%=0
�� orbit= 0.1 � 2.5 � 0.05
�C%=C%+1
��GCOL 0,C%
�
U=orbit/3
�
V=orbit/3
�� B%= 1 � 300
�"� �(U)>1E6 � �(V)>1E6 � � �dp@
� � 69,(U*640)+640,(V*512)+512
�X=U*cosA-(V-U*U)*sinA
�Y=U*sinA+(V-U*U)*cosA
�U=X:V=Y
��
��

!� �0,0)"This is A = ";A;�(18)


� �0,31);

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�

00000000  0d 00 0a 22 f4 20 3e 20  3c 42 61 73 69 63 53 61  |...". > <BasicSa|
00000010  76 65 24 64 69 72 3e 2e  4b 41 4d 5f 41 54 52 41  |ve$dir>.KAM_ATRA|
00000020  43 54 0d 00 14 1b f1 22  53 74 72 61 6e 67 65 20  |CT....."Strange |
00000030  41 74 74 72 61 63 74 6f  72 73 20 31 22 0d 00 1e  |Attractors 1"...|
00000040  18 f1 22 54 68 65 20 4b  41 4d 20 61 74 74 72 61  |.."The KAM attra|
00000050  63 74 6f 72 22 0d 00 28  13 f1 22 42 79 20 4d 69  |ctor"..(.."By Mi|
00000060  6b 65 20 43 6f 6f 6b 22  0d 00 32 32 f1 22 41 20  |ke Cook"..22."A |
00000070  64 65 66 69 6e 65 73 20  74 68 65 20 41 6e 67 6c  |defines the Angl|
00000080  65 20 6f 66 20 74 68 65  20 6f 72 62 69 74 20 69  |e of the orbit i|
00000090  6e 20 72 61 64 69 61 6e  73 22 0d 00 3c 05 f5 0d  |n radians"..<...|
000000a0  00 46 30 e8 22 45 6e 74  65 72 20 61 20 76 61 6c  |.F0."Enter a val|
000000b0  75 65 20 66 6f 72 20 41  20 61 62 6f 75 74 20 28  |ue for A about (|
000000c0  31 2e 31 20 74 6f 20 31  2e 37 29 20 22 2c 41 0d  |1.1 to 1.7) ",A.|
000000d0  00 50 06 eb 30 0d 00 5a  2c f1 20 8a 30 2c 30 29  |.P..0..Z,. .0,0)|
000000e0  3b 22 54 68 65 20 4b 41  4d 20 61 74 74 72 61 63  |;"The KAM attrac|
000000f0  74 6f 72 20 42 79 20 4d  69 6b 65 20 43 6f 6f 6b  |tor By Mike Cook|
00000100  22 0d 00 64 0d 73 69 6e  41 3d b5 28 41 29 0d 00  |"..d.sinA=.(A)..|
00000110  6e 0d 63 6f 73 41 3d 9b  28 41 29 0d 00 78 08 43  |n.cosA=.(A)..x.C|
00000120  25 3d 30 0d 00 82 1d e3  20 6f 72 62 69 74 3d 20  |%=0..... orbit= |
00000130  30 2e 31 20 b8 20 32 2e  35 20 88 20 30 2e 30 35  |0.1 . 2.5 . 0.05|
00000140  0d 00 8c 0b 43 25 3d 43  25 2b 31 0d 00 96 0e f4  |....C%=C%+1.....|
00000150  47 43 4f 4c 20 30 2c 43  25 0d 00 a0 0d 55 3d 6f  |GCOL 0,C%....U=o|
00000160  72 62 69 74 2f 33 0d 00  aa 0d 56 3d 6f 72 62 69  |rbit/3....V=orbi|
00000170  74 2f 33 0d 00 b4 11 e3  20 42 25 3d 20 31 20 b8  |t/3..... B%= 1 .|
00000180  20 33 30 30 0d 00 be 22  e7 20 94 28 55 29 3e 31  | 300...". .(U)>1|
00000190  45 36 20 84 20 94 28 56  29 3e 31 45 36 20 8c 20  |E6 . .(V)>1E6 . |
000001a0  e5 20 8d 64 70 40 0d 00  c8 20 f0 20 36 39 2c 28  |. .dp@... . 69,(|
000001b0  55 2a 36 34 30 29 2b 36  34 30 2c 28 56 2a 35 31  |U*640)+640,(V*51|
000001c0  32 29 2b 35 31 32 0d 00  d2 19 58 3d 55 2a 63 6f  |2)+512....X=U*co|
000001d0  73 41 2d 28 56 2d 55 2a  55 29 2a 73 69 6e 41 0d  |sA-(V-U*U)*sinA.|
000001e0  00 dc 19 59 3d 55 2a 73  69 6e 41 2b 28 56 2d 55  |...Y=U*sinA+(V-U|
000001f0  2a 55 29 2a 63 6f 73 41  0d 00 e6 0b 55 3d 58 3a  |*U)*cosA....U=X:|
00000200  56 3d 59 0d 00 f0 05 ed  0d 00 fa 05 ed 0d 01 04  |V=Y.............|
00000210  21 f1 20 8a 30 2c 30 29  22 54 68 69 73 20 69 73  |!. .0,0)"This is|
00000220  20 41 20 3d 20 22 3b 41  3b 89 28 31 38 29 0d 01  | A = ";A;.(18)..|
00000230  0e 0d f1 20 8a 30 2c 33  31 29 3b 0d 01 18 07 fd  |... .0,31);.....|
00000240  20 a3 0d ff                                       | ...|
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