394c160e-fb4e-43c6-aceb-3e4a84fe235d 10 4 5 decimal

&[DATE] &[TIME] - &[FILENAME]

Analysis of Gyroscopic Rotors:

Z 22 matrix :

IC 41 matrix :

I 2 identity :

IC 1 el 0.01 :

I.A 0.11 :

J 0.084 :

Ω 62.2 :

k 13.416 106^* :

l.0 63103 -^* :

G 0 J Ω * J Ω * - 022 mat :

M I.A 00 I.A 22 mat :

K k l.0 2^* 00 k l.0 2^* 22 mat :

B K G Z I - 22 mat :

A Z M I Z 22 mat :

A Z I stack M Z stack augment :

B K Z stack G I - stack augment :

t Φ D A invert B * Φ 1 el Φ 2 el Φ 3 el Φ 4 el 41 mat * - :

S IC 051000 t Φ D Adams :

S #

t Φ D 0011100 / 000011100 / 1000010044 mat invert 6656013125 / 0065311250 / 06656013125 / 65311250 / - 0001 - 00001 - 44 mat * Φ 1 el Φ 2 el Φ 3 el Φ 4 el 41 mat * -

sol IC 015000 t Φ D dn_AdamsMoulton :

sol 0 0.01 000 0.0002 0.0099 3.0594 107 -^* - 0.965 - 0.0046 - 0.0004 0.0096 2.4334 106 -^* - 1.9113 - 0.0182 - 0.0006 0.0091 8.1326 106 -^* - 2.8204 - 0.0402 - 0.0008 0.0085 1.9014 105 -^* - 3.6748 - 0.0698 - 0.001 0.0077 3.6486 105 -^* - 4.4579 - 0.1059 - 0.0012 0.0067 6.1694 105 -^* - 5.1544 - 0.1469 - 0.0014 0.0056 9.5472 105 -^* - 5.7508 - 0.1913 - 0.0016 0.0044 0.0001 - 6.2357 - 0.2371 - 0.0018 0.0031 0.0002 - 6.5995 - 0.2823 - 105 mat

G1 sol 1 col sol 2 col augment : G2 sol 1 col sol 3 col augment : G3 sol 1 col sol 4 col augment : G4 sol 1 col sol 5 col augment : 41 sys

G1 101 row G2 101 row G3 101 row G4 101 row 41 mat 0.02 0.002 12 mat 0.02 0.0007 12 mat 0.02 6.0411 - 12 mat 0.02 3.1076 - 12 mat 41 mat

G1 1 1 sys G2 1 1 sys G3 1 1 sys G4 1 1 sys