studephm (Материалы и задания к курсовой работе), страница 6
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Текстовый-файл из архива "Материалы и задания к курсовой работе", который расположен в категории "". Всё это находится в предмете "системы управления и передачи информации" из 10 семестр (2 семестр магистратуры), которые можно найти в файловом архиве МАИ. Не смотря на прямую связь этого архива с МАИ, его также можно найти и в других разделах. Архив можно найти в разделе "курсовые/домашние работы", в предмете "системы управления и передачи информации" в общих файлах.
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E = 4.2862819973379370e-003 [ - ]
Roota = 5.1536262779235840e+003 [ meters**1/2 ]
Toe = 230400 [ sec ]
Cic = 0.0000000000000000e+000 [ radians ]
Crc = 2.2965625000000000e+002 [ meters ]
Cis = 3.5390257835388180e-008 [ radians ]
Crs = 7.1250000000000000e+000 [ meters ]
Cuc = 1.8440186977386470e-007 [ radians ]
Cus = 6.7241489887237550e-006 [ radians ]
Omega0 = 8.7309854896739130e-001 [ semicircle ]
Omega = -9.0283821010962130e-001 [ semicircle ]
I0 = 2.9518128419294950e-001 [ semicircle ]
Omegadot= -2.7366695576347410e-009 [ semicircle/sec ]
Idot = -5.1727511163335290e-011 [ semicircle/sec ]
Accuracy= 7 [ coded ]
Health = 0 [ coded ]
Fit= 0 [ coded ]
********* Satellite number : 47 (15) ***********
Litera = 4 [ - ]
Tk = 61200 [ sec ]
Day = 1031 [ days ]
Tb = 62100 [ sec ]
Gn = -5.4569682106375690e-012 [ sec/sec ]
Tn = -7.0352107286453250e-005 [ sec ]
X = 1.0134324707031250e+004 [ km ]
Y = 3.9905307617187500e+003 [ km ]
Z = 2.3044091308593750e+004 [ km ]
Xt = -8.4912586212158200e-001 [ km/sec ]
Yt = 3.0455636978149410e+000 [ km/sec ]
Zt = -1.6141033172607420e-001 [ km/sec ]
Xtt= 0.0000000000000000e+000 [ km/sec**2 ]
Ytt= 0.0000000000000000e+000 [ km/sec**2 ]
Ztt= -2.7939677238464360e-009 [ km/sec**2 ]
Tc = -3.8743019104003910e-007 [ sec ]
Age = 1 [ days ]
Flags = 13 [ - ]
Health = 0 [ 0 - o'k ]
************* Satellite number : 26 *************
Wn = 981 [ week ]
Tow = 223200 [ sec ]
Tgd = 0.0000000000000000e+000 [ sec ]
Aodc = 733 [ - ]
Toc = 230400 [ sec ]
Af2 = 0.0000000000000000e+000 [ sec/sec**2 ]
Af1 = 4.1495695768389850e-011 [ sec/sec ]
Af0 = 5.8042351156473160e-004 [ sec ]
Aode = 221 [ - ]
Deltan = 1.4777015167055650e-009 [ semicircle/sec ]
M0 = 7.9460688866674900e-001 [ semicircle ]
E = 1.0685553308576350e-002 [ - ]
Roota = 5.1537150936126710e+003 [ meters**1/2 ]
Toe = 230400 [ sec ]
Cic = -1.6763806343078610e-007 [ radians ]
Crc = 1.9156250000000000e+002 [ meters ]
Cis = 2.5704503059387210e-007 [ radians ]
Crs = -3.4468750000000000e+001 [ meters ]
Cuc = -1.5646219253540040e-006 [ radians ]
Cus = 9.7379088401794430e-006 [ radians ]
Omega0 = 5.6095999339595440e-001 [ semicircle ]
Omega = -4.4929439201951030e-002 [ semicircle ]
I0 = 3.0531523516401650e-001 [ semicircle ]
Omegadot= -2.5180497686960730e-009 [ semicircle/sec ]
Idot = 7.9353412729687990e-011 [ semicircle/sec ]
Accuracy= 7 [ coded ]
Health = 0 [ coded ]
Fit= 0 [ coded ]
************* Satellite number : 27 *************
Wn = 981 [ week ]
Tow = 223200 [ sec ]
Tgd = 4.6566128730773930e-010 [ sec ]
Aodc = 355 [ - ]
Toc = 230400 [ sec ]
Af2 = 0.0000000000000000e+000 [ sec/sec**2 ]
Af1 = 1.2505552149377760e-012 [ sec/sec ]
Af0 = 2.9988586902618410e-007 [ sec ]
Aode = 99 [ - ]
Deltan = 1.6768808563938360e-009 [ semicircle/sec ]
M0 = -1.3079403480514880e-001 [ semicircle ]
E = 1.2975813238881530e-002 [ - ]
Roota = 5.1537372932434080e+003 [ meters**1/2 ]
Toe = 230400 [ sec ]
Cic = 2.5518238544464110e-007 [ radians ]
Crc = 2.3356250000000000e+002 [ meters ]
Cis = 2.0489096641540530e-008 [ radians ]
Crs = 8.9687500000000000e+000 [ meters ]
Cuc = 3.2223761081695560e-007 [ radians ]
Cus = 6.9700181484222410e-006 [ radians ]
Omega0 = 8.8384620985016230e-001 [ semicircle ]
Omega = -9.6151975123211740e-001 [ semicircle ]
I0 = 2.9950400581583380e-001 [ semicircle ]
Omegadot= -2.6957422960549590e-009 [ semicircle/sec ]
Idot = -4.3769432522822170e-011 [ semicircle/sec ]
Accuracy= 7 [ coded ]
Health = 0 [ coded ]
Fit= 0 [ coded ]
************* Satellite number : 31 *************
Wn = 981 [ week ]
Tow = 223200 [ sec ]
Tgd = 1.3969838619232180e-009 [ sec ]
Aodc = 385 [ - ]
Toc = 230400 [ sec ]
Af2 = 0.0000000000000000e+000 [ sec/sec**2 ]
Af1 = 5.6843418860808010e-013 [ sec/sec ]
Af0 = 8.6547806859016420e-006 [ sec ]
Aode = 129 [ - ]
Deltan = 1.4191527952789330e-009 [ semicircle/sec ]
M0 = 4.9921647319570180e-001 [ semicircle ]
E = 8.2319132052361970e-003 [ - ]
Roota = 5.1536575641632080e+003 [ meters**1/2 ]
Toe = 230400 [ sec ]
Cic = -1.3411045074462890e-007 [ radians ]
Crc = 2.4337500000000000e+002 [ meters ]
Cis = 2.4214386940002440e-008 [ radians ]
Crs = 5.8187500000000000e+001 [ meters ]
Cuc = 3.0193477869033810e-006 [ radians ]
Cus = 7.0314854383468630e-006 [ radians ]
Omega0 = -4.4494971120730040e-001 [ semicircle ]
Omega = 2.3833443177863960e-001 [ semicircle ]
I0 = 3.0452847527340050e-001 [ semicircle ]
Omegadot= -2.6116140361409630e-009 [ semicircle/sec ]
Idot = -1.3301360013429080e-011 [ semicircle/sec ]
Accuracy= 7 [ coded ]
Health = 0 [ coded ]
Fit= 0 [ coded ]
********* Satellite number : 49 (17) ***********
Litera = 24 [ - ]
Tk = 61200 [ sec ]
Day = 1031 [ days ]
Tb = 62100 [ sec ]
Gn = -3.6379788070917130e-012 [ sec/sec ]
Tn = 1.3442710041999820e-004 [ sec ]
X = 1.5151387207031250e+004 [ km ]
Y = 1.9357877929687500e+004 [ km ]
Z = 6.8745341796875000e+003 [ km ]
Xt = -5.7783699035644530e-001 [ km/sec ]
Yt = -7.5408458709716800e-001 [ km/sec ]
Zt = 3.3948373794555660e+000 [ km/sec ]
Xtt= 9.3132257461547850e-010 [ km/sec**2 ]
Ytt= 9.3132257461547850e-010 [ km/sec**2 ]
Ztt= -1.8626451492309570e-009 [ km/sec**2 ]
Tc = -3.8743019104003910e-007 [ sec ]
Age = 0 [ days ]
Flags = 13 [ - ]
Health = 0 [ 0 - o'k ]
End of file.