Project Soyuz 7k.dll

castorp

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The aft engines also seem to be angled inward a lot:

3492f45f491fa45ff26f1debbd91_grande.jpg

ja ja ja...
;-)
that's a known (and old) error in the PAO mesh that i never got around to correcting...
'will add it to the to-do list.
'any ideas/guesses as to what the actual angle off of the axis for those aft engines is supposed to be?
 

N_Molson

Addon Developer
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Lift to drag should be 0.4 (constant ratio until subsonic speeds)

Here's what I get :

Code:
Orbiter Flight Data Log Record
==============================
Columns:
	TIME:     simulation time (seconds)
	ALT:      altitude (km)
	AIRSPEED: airspeed (m/s)
	MACH:     Mach number
	TEMP:     freestream temperature (K)
	STP:      static pressure (kPa)
	DNP:      dynamic pressure (kPa)
	AOA:      angle of attack (deg)
	SLIP:     horizontal slip angle (deg)
	LIFT:     total lift force (kN)
	DRAG:     total drag force (kN)
	L/D:      lift/drag ratio
	MASS:     vessel mass (kg)

# Log started for Soyuz-12
# ____TIME _____L/D _______ALT __MACH ____AOA ___SLIP
     30.90    0.009    95.3272  27.65   179.1  -175.6
     31.90    0.009    95.1799  27.65   179.1  -175.6
     32.90    0.008    95.0326  27.66   179.1  -175.7
     33.91    0.008    94.8851  27.66   179.1  -175.7
     34.91    0.008    94.7400  27.67   179.1  -175.7
     35.91    0.008    94.5916  27.67   179.2  -175.7
     36.91    0.008    94.4444  27.68   179.2  -175.7
     37.92    0.007    94.2982  27.68   179.2  -175.8
     38.92    0.007    94.1508  27.69   179.2  -175.8
     39.93   -0.001    94.0042  27.69  -179.8  -175.8
     40.94   -0.028    93.8572  27.69  -177.1  -175.8
     41.94   -0.075    93.7104  27.70  -172.1  -175.8
     42.94   -0.125    93.5645  27.70  -166.8  -175.8
     43.94   -0.170    93.4188  27.70  -162.0  -175.7
     44.95   -0.178    93.2727  27.71  -161.2  -175.7
     45.95   -0.185    93.1267  27.71  -160.4  -175.6
     46.96   -0.187    92.9809  27.71  -159.8  -175.6
     47.97   -0.188    92.8351  27.71  -159.9  -175.6
     48.97   -0.185    92.6901  27.72  -159.5  -175.6
     49.97   -0.186    92.5449  27.72  -159.6  -175.6
     50.98   -0.186    92.3995  27.72  -159.7  -175.7
     51.98   -0.181    92.2548  27.72  -159.1  -175.6
     52.99   -0.178    92.1103  27.72  -158.8  -175.6
     53.99   -0.179    91.9653  27.73  -158.8  -175.6
     54.99   -0.176    91.8212  27.73  -158.5  -175.6
     55.99   -0.176    91.6771  27.73  -158.6  -175.7
     57.00   -0.177    91.5326  27.73  -158.7  -175.7
     58.00   -0.178    91.3885  27.73  -158.8  -175.7
     59.01   -0.179    91.2444  27.73  -158.9  -175.7
     60.01   -0.181    91.1005  27.73  -159.1  -175.7
     61.01   -0.182    90.9573  27.74  -159.2  -175.7
     62.01   -0.184    90.8143  27.74  -159.4  -175.8
     63.02   -0.186    90.6713  27.74  -159.6  -175.8
     64.02   -0.188    90.5276  27.74  -159.8  -175.8
     65.03   -0.188    90.3845  27.74  -159.9  -175.8
     66.03   -0.189    90.2415  27.74  -160.0  -175.8
     67.04   -0.189    90.0987  27.74  -160.1  -175.8
     68.04   -0.188    89.9558  27.74  -160.1  -175.8
     69.04   -0.187    89.8148  27.74  -160.2  -175.8
     70.05   -0.187    89.6718  27.74  -160.2  -175.8
     71.05   -0.186    89.5295  27.74  -160.3  -175.8
     72.05   -0.186    89.3880  27.74  -160.3  -175.9
     73.06   -0.185    89.2458  27.74  -159.5  -175.8
     74.07   -0.185    89.1031  27.74  -159.6  -175.8
     75.07   -0.188    88.9619  27.74  -159.9  -175.9
     76.07   -0.189    88.8208  27.74  -160.0  -175.9
     77.08   -0.189    88.6797  27.74  -160.0  -175.9
     78.08   -0.189    88.5388  27.74  -160.0  -175.9
     79.08   -0.188    88.3985  27.74  -160.1  -175.9
     80.09   -0.187    88.2576  27.74  -160.2  -175.9
     81.09   -0.186    88.1180  27.74  -160.3  -175.9
     82.09   -0.185    87.9767  27.74  -160.5  -176.0
     83.10   -0.183    87.8370  27.74  -160.6  -176.0
     84.11   -0.182    87.6968  27.74  -160.8  -176.0
     85.11   -0.187    87.5566  27.74  -160.3  -176.1
     86.12   -0.188    87.4165  27.74  -160.2  -176.1
     87.13   -0.187    87.2757  27.74  -160.2  -176.1
     88.14   -0.187    87.1351  27.74  -160.3  -176.1
     89.15   -0.188    86.9956  27.74  -159.8  -176.1
     90.15   -0.183    86.8563  27.74  -159.3  -176.1
     91.16   -0.187    86.7166  27.74  -160.2  -176.1
     92.17   -0.187    86.5772  27.74  -160.3  -176.1
     93.18   -0.188    86.4380  27.74  -160.1  -176.1
     94.19   -0.188    86.2992  27.74  -160.1  -176.1
     95.19   -0.188    86.1606  27.74  -160.2  -176.1
     96.20   -0.187    86.0224  27.74  -160.2  -176.1
     97.21   -0.186    85.8833  27.80  -160.3  -176.1
     98.21   -0.186    85.7457  27.78  -160.4  -176.1
     99.22   -0.185    85.6081  27.76  -160.4  -176.1
    100.23   -0.188    85.4696  27.74  -160.1  -176.1
    101.24   -0.187    85.3320  27.72  -160.2  -176.1
    102.24   -0.187    85.1960  27.70  -160.2  -176.1
    103.24   -0.189    85.0582  27.68  -160.0  -176.1
    104.25   -0.189    84.9213  27.66  -160.0  -176.1
    105.26   -0.188    84.7849  27.64  -160.1  -176.2
    106.41   -0.187    84.6480  27.62  -160.2  -176.2
    107.42   -0.186    84.4907  27.60  -160.3  -176.2
    108.42   -0.189    84.3549  27.58  -160.0  -176.2
    109.43   -0.188    84.2190  27.56  -160.1  -176.2
    110.44   -0.188    84.0822  27.54  -160.2  -176.2
    111.44   -0.188    83.9473  27.52  -160.2  -176.2
    112.45   -0.187    83.8116  27.50  -160.3  -176.3
    113.46   -0.187    83.6753  27.48  -160.2  -176.3
    114.46   -0.188    83.5404  27.46  -160.2  -176.3
    115.47   -0.188    83.4068  27.44  -160.1  -176.3
    116.47   -0.189    83.2716  27.42  -160.1  -176.3
    117.47   -0.188    83.1376  27.40  -160.1  -176.3
    118.48   -0.189    83.0033  27.38  -160.1  -176.3
    119.49   -0.188    82.8677  27.36  -160.1  -176.3
    120.50   -0.189    82.7336  27.34  -160.1  -176.3
    121.51   -0.189    82.5996  27.32  -160.0  -176.3
    122.51   -0.189    82.4665  27.30  -160.0  -176.3
    123.51   -0.189    82.3336  27.28  -160.0  -176.3
    124.52   -0.189    82.2005  27.27  -160.0  -176.3
    125.52   -0.188    82.0680  27.25  -160.1  -176.3
    126.52   -0.189    81.9357  27.23  -160.0  -176.3
    127.53   -0.189    81.8021  27.21  -160.1  -176.3
    128.54   -0.189    81.6695  27.19  -160.0  -176.3
    129.55   -0.189    81.5373  27.17  -160.1  -176.3
    130.56   -0.189    81.4041  27.15  -160.0  -176.3
    131.56   -0.189    81.2731  27.13  -160.0  -176.3
    132.56   -0.189    81.1425  27.11  -160.0  -176.4
    133.57   -0.189    81.0101  27.10  -160.0  -176.4
    134.58   -0.189    80.8787  27.08  -160.0  -176.4
    135.58   -0.189    80.7474  27.06  -160.0  -176.4
    136.59   -0.189    80.6170  27.04  -160.0  -176.4
    137.60   -0.188    80.4859  27.02  -160.1  -176.4
    138.60   -0.188    80.3566  27.00  -160.1  -176.4
    139.60   -0.189    80.2264  26.98  -160.1  -176.4
    140.60   -0.189    80.0969  26.96  -160.1  -176.4
    141.60   -0.189    79.9678  26.95  -160.1  -176.4
    142.61   -0.188    79.8381  26.93  -160.1  -176.4
    143.62   -0.189    79.7087  26.91  -160.0  -176.4
    144.63   -0.189    79.5792  26.89  -160.0  -176.4
    145.63   -0.189    79.4501  26.87  -160.0  -176.4
    146.64   -0.189    79.3218  26.85  -160.0  -176.4
    147.65   -0.189    79.1935  26.83  -160.0  -176.4
    148.65   -0.189    79.0653  26.82  -160.0  -176.4
    149.65   -0.189    78.9376  26.80  -160.0  -176.4
    150.65   -0.189    78.8111  26.78  -160.0  -176.4
    151.65   -0.189    78.6833  26.76  -160.0  -176.4
    152.65   -0.189    78.5564  26.74  -159.9  -176.4
    153.66   -0.188    78.4295  26.72  -159.9  -176.5
    154.66   -0.187    78.3028  26.71  -159.8  -176.5
    155.67   -0.187    78.1765  26.69  -159.7  -176.5
    156.68   -0.186    78.0496  26.67  -159.7  -176.5
    157.68   -0.187    77.9234  26.65  -159.8  -176.5
    158.69   -0.188    77.7970  26.63  -159.9  -176.5
    159.70   -0.189    77.6710  26.61  -159.9  -176.5
    160.71   -0.189    77.5448  26.59  -160.0  -176.5
    161.72   -0.189    77.4191  26.58  -160.0  -176.5
    162.72   -0.188    77.2949  26.56  -159.9  -176.5
    163.73   -0.188    77.1692  26.54  -159.9  -176.5
    164.74   -0.189    77.0444  26.52  -160.0  -176.5
    165.75   -0.188    76.9208  26.50  -159.9  -176.5
    166.75   -0.189    76.7967  26.48  -160.0  -176.5
    167.75   -0.189    76.6728  26.47  -160.1  -176.5
    168.76   -0.188    76.5500  26.45  -160.1  -176.5
    169.77   -0.188    76.4254  26.43  -160.1  -176.5
    170.78   -0.188    76.3021  26.41  -160.1  -176.5
    171.79   -0.188    76.1784  26.39  -160.1  -176.6
    172.80   -0.188    76.0555  26.37  -160.2  -176.6
    173.80   -0.187    75.9335  26.36  -160.2  -176.6
    174.81   -0.187    75.8112  26.34  -160.3  -176.6
    175.83   -0.188    75.6891  26.32  -160.2  -176.6
    176.83   -0.188    75.5669  26.30  -160.1  -176.6
    177.84   -0.189    75.4454  26.28  -160.0  -176.6
    178.85   -0.188    75.3241  26.26  -160.1  -176.6
    179.85   -0.188    75.2036  26.25  -160.2  -176.6
    180.85   -0.188    75.0840  26.23  -160.1  -176.6
    181.86   -0.188    74.9641  26.21  -160.1  -176.6
    182.87   -0.189    74.8445  26.19  -160.1  -176.6
    183.87   -0.188    74.7243  26.17  -160.1  -176.6
    184.88   -0.188    74.6055  26.15  -160.2  -176.6
    185.88   -0.189    74.4859  26.13  -160.1  -176.6
    186.89   -0.188    74.3675  26.12  -160.1  -176.6
    187.89   -0.188    74.2487  26.10  -160.2  -176.6
    188.90   -0.188    74.1307  26.08  -160.1  -176.6
    189.91   -0.189    74.0123  26.06  -160.1  -176.7
    190.91   -0.189    73.8949  26.04  -160.0  -176.7
    191.92   -0.188    73.7774  26.02  -160.1  -176.7
    192.92   -0.188    73.6607  26.00  -160.2  -176.7
    193.93   -0.188    73.5444  25.99  -160.2  -176.7
    194.93   -0.189    73.4276  25.97  -160.0  -176.7
    195.94   -0.189    73.3116  25.95  -160.0  -176.7
    196.95   -0.189    73.1946  25.93  -160.1  -176.7
    197.96   -0.188    73.0783  25.91  -160.1  -176.7
    198.97   -0.189    72.9631  25.89  -160.1  -176.7
    199.97   -0.189    72.8484  25.87  -160.0  -176.7
    200.97   -0.189    72.7337  25.85  -160.0  -176.7
    201.97   -0.189    72.6197  25.84  -159.9  -176.7
    202.98   -0.189    72.5058  25.82  -159.9  -176.7
    203.98   -0.189    72.3924  25.80  -160.0  -176.7
    204.99   -0.189    72.2791  25.78  -160.0  -176.8
    205.99   -0.189    72.1663  25.76  -160.0  -176.8
    206.99   -0.189    72.0542  25.74  -160.0  -176.8
    208.00   -0.189    71.9412  25.73  -160.0  -176.8
    209.00   -0.188    71.8296  25.70  -160.1  -176.8
    210.00   -0.188    71.7175  25.68  -160.2  -176.8
    211.01   -0.188    71.6064  25.66  -160.1  -176.8
    212.02   -0.188    71.4948  25.63  -160.1  -176.8
    213.02   -0.188    71.3843  25.61  -160.1  -176.8
    214.03   -0.189    71.2732  25.58  -160.0  -176.8
    215.03   -0.188    71.1635  25.56  -159.9  -176.8
    216.03   -0.189    71.0540  25.53  -160.0  -176.8
    217.04   -0.188    70.9439  25.51  -160.1  -176.8
    218.05   -0.187    70.8348  25.48  -160.2  -176.9
    219.05   -0.187    70.7254  25.46  -160.3  -176.9
    220.05   -0.187    70.6170  25.44  -160.2  -176.9
    221.06   -0.189    70.5084  25.41  -160.1  -176.9
    222.07   -0.188    70.4005  25.39  -160.1  -176.9
    223.08   -0.188    70.2924  25.36  -160.2  -176.9
    224.08   -0.189    70.1848  25.34  -160.0  -176.9
    225.10   -0.189    70.0774  25.31  -160.1  -176.9
    226.11   -0.189    69.9695  25.29  -160.0  -176.9
    227.12   -0.188    69.8635  25.26  -160.2  -176.9
    228.13   -0.188    69.7571  25.24  -160.2  -176.9
    229.13   -0.189    69.6518  25.21  -160.1  -176.9
    230.14   -0.189    69.5459  25.19  -160.0  -176.9
    231.14   -0.188    69.4414  25.16  -160.1  -177.0
    232.15   -0.189    69.3367  25.14  -160.0  -177.0
    233.15   -0.189    69.2329  25.12  -160.0  -177.0
    234.16   -0.189    69.1286  25.09  -159.9  -177.0
    235.17   -0.189    69.0253  25.07  -159.9  -177.0
    236.18   -0.188    68.9215  25.04  -159.8  -177.0
    237.18   -0.187    68.8186  25.02  -159.7  -177.0
    238.19   -0.188    68.7164  24.99  -159.8  -177.0
    239.20   -0.189    68.6141  24.97  -160.0  -177.0
    239.72   -0.189    68.5611  24.95  -160.0  -177.0
    240.72   -0.188    68.4596  24.93  -160.1  -177.0
    241.73   -0.189    68.3586  24.90  -160.0  -177.0
    242.73   -0.189    68.2585  24.88  -160.0  -177.0
    243.74   -0.189    68.1574  24.85  -160.0  -177.1
    244.75   -0.189    68.0569  24.83  -160.0  -177.1
    245.75   -0.189    67.9571  24.80  -160.0  -177.1
    246.76   -0.189    67.8576  24.78  -160.0  -177.1
    247.77   -0.189    67.7584  24.75  -160.0  -177.1
    248.77   -0.189    67.6601  24.73  -160.0  -177.1
    249.78   -0.189    67.5614  24.70  -160.0  -177.1
    250.79   -0.189    67.4633  24.68  -160.0  -177.1
    251.80   -0.189    67.3651  24.65  -160.0  -177.1
    252.81   -0.189    67.2679  24.62  -160.0  -177.1
    253.81   -0.189    67.1718  24.60  -160.0  -177.1
    254.82   -0.189    67.0745  24.57  -159.9  -177.1
    255.83   -0.189    66.9784  24.55  -159.9  -177.2
    256.83   -0.189    66.8831  24.52  -160.0  -177.2
    257.83   -0.189    66.7877  24.50  -160.0  -177.2
    258.84   -0.189    66.6933  24.47  -160.0  -177.2
    259.84   -0.189    66.5987  24.44  -160.0  -177.2
    260.85   -0.189    66.5048  24.42  -160.0  -177.2
    261.85   -0.189    66.4105  24.39  -160.0  -177.2
    262.86   -0.189    66.3165  24.37  -160.0  -177.2
    263.88   -0.189    66.2229  24.34  -160.0  -177.2
    264.89   -0.189    66.1296  24.31  -160.0  -177.2
    265.90   -0.189    66.0367  24.29  -160.0  -177.3
    266.91   -0.189    65.9442  24.26  -159.9  -177.3
    267.93   -0.188    65.8525  24.23  -159.9  -177.3
    268.94   -0.188    65.7599  24.21  -159.8  -177.3
    269.95   -0.189    65.6693  24.18  -160.0  -177.3
    270.95   -0.189    65.5783  24.15  -160.0  -177.3
    271.95   -0.189    65.4886  24.13  -160.0  -177.3
    272.96   -0.188    65.3986  24.10  -160.1  -177.3
    273.97   -0.188    65.3088  24.07  -160.1  -177.3
    274.97   -0.188    65.2197  24.05  -160.1  -177.3
    275.98   -0.189    65.1309  24.02  -160.1  -177.4
    276.99   -0.189    65.0423  23.99  -160.0  -177.4
    278.00   -0.189    64.9540  23.97  -160.0  -177.4
    279.00   -0.189    64.8661  23.94  -160.0  -177.4
    280.01   -0.189    64.7789  23.91  -160.0  -177.4
    281.02   -0.189    64.6917  23.89  -160.0  -177.4
    282.02   -0.189    64.6054  23.86  -160.0  -177.4
    283.02   -0.189    64.5207  23.83  -160.0  -177.4
    284.03   -0.189    64.4336  23.80  -160.0  -177.4
    285.03   -0.189    64.3485  23.78  -160.0  -177.5
    286.04   -0.189    64.2631  23.75  -160.0  -177.5
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    560.59   -0.098    34.0483   9.32  -169.7  -179.2
    561.59   -0.097    33.8313   9.20  -169.8  -179.2
    562.78   -0.078    33.6371   9.09  -172.0  -179.4
    563.78   -0.004    33.3516   8.93  -179.7  -180.0
    564.78    0.058    33.1265   8.81   173.9   179.6
    565.79    0.095    32.8928   8.71   170.0   179.2
    566.80    0.092    32.6496   8.57   170.3   179.2
    567.80    0.051    32.4004   8.44   174.7   179.4
    568.81   -0.013    32.1435   8.30  -178.5   179.8
    569.82   -0.072    31.8827   8.16  -172.4  -179.7
    570.82   -0.098    31.6220   8.03  -169.7  -179.3
    571.82   -0.083    31.3624   7.89  -171.3  -179.2
    572.82   -0.033    31.1043   7.75  -176.6  -179.3
    573.83    0.035    30.8391   7.61   176.3  -179.7
    574.84    0.086    30.5688   7.47   170.9   179.8
    575.84    0.099    30.2938   7.33   169.6   179.4
    576.85    0.069    30.0094   7.19   172.8   179.2
    577.86    0.008    29.7201   7.05   179.2   179.2
    578.87   -0.058    29.4259   6.91  -173.9   179.6
    579.87   -0.096    29.1341   6.77  -169.8  -179.9
    580.87   -0.093    28.8446   6.62  -170.2  -179.5
    581.88   -0.049    28.5570   6.48  -174.9  -179.2
    582.88    0.019    28.2696   6.34   177.9  -179.1
    583.88    0.078    27.9788   6.20   171.8  -179.4
    584.88    0.103    27.6815   6.06   169.2  -179.9
    585.89    0.083    27.3770   5.91   171.4   179.6
    586.90    0.025    27.0669   5.77   177.4   179.2
    587.91   -0.045    26.7561   5.63  -175.2   179.1
    588.91   -0.094    26.4471   5.49  -170.1   179.3
    589.92   -0.102    26.1402   5.35  -169.3   179.8
    590.92   -0.067    25.8381   5.21  -173.0  -179.7
    591.93   -0.001    25.5370   5.07   180.0  -179.2
    592.93    0.067    25.2356   4.94   172.9  -179.0
# Log stopped for Soyuz-12
 

Urwumpe

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So you have too little lift.
 

N_Molson

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So you have too little lift.

Wow, I wasn't thinking that such a shape could generate that much lift !

But it fits with the "double dip" reentries techniques like Komarov did on Soyuz-1, with that much lift I guess you can bounce, then get a steeper reentry angle.
 

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Wow, I wasn't thinking that such a shape could generate that much lift !

But it fits with the "double dip" reentries techniques like Komarov did on Soyuz-1, with that much lift I guess you can bounce, then get a steeper reentry angle.

Yes, but 0.4 L/D at supersonic speeds isn't that good at all, it is a fairly good value for a capsule (even slightly better than Apollo), but the Shuttle for example had an L/D of 1.6, Buran should even have been slightly better because of the optimized tile placement.
 

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Corrected the lift coefficients, it works, it is possible to make a small "bounce" and of course allows much more control on the capsule trajectory.

(constant ratio until subsonic speeds)

I think that the capsule currently "stalls" around Mach 8-9. What's the way to correct this, wing aspect ?
 

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N_Molson

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It's because the RCS thrusters are overrun by the aerodynamic moment. So I should reduce that moment coefficients so that the thrusters can keep 20° of AOA until Mach 1 ? Also, do you know if there is a "lower altitude limit" for the use of those peroxyde thrusters ?
 

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It's because the RCS thrusters are overrun by the aerodynamic moment. So I should reduce that moment coefficients so that the thrusters can keep 20° of AOA until Mach 1 ? Also, do you know if there is a "lower altitude limit" for the use of those peroxyde thrusters ?

They should have a pretty strong dependency on atmospheric pressure, but it doesn't really matter, they should produce enough thrust for small maneuvers even at sea level.

And your moment function is then completely wrong - at 20° AOA you should have 0 Nm torque by aerodynamics. Any deviation from 20° would get corrected with relative weak moments, but if you have enough dynamic pressure for 4g deceleration, even weak moments will rotate you into the right orientation in less than 3 seconds.
 

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Got a prob in docking. Probe is deployed, but the Soyuz goes right past the docking target, no capture. Using majortom's Salyut 6.

Edit: Tryed the "docked" scn. I undocked and re-docked. Probe deployed, I dock, and when I retract the probe, the HUD says there is hard-dock, but the Soyuz starts to fly away.
 
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N_Molson

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Edit: Tryed the "docked" scn. I undocked and re-docked. Probe deployed, I dock, and when I retract the probe, the HUD says there is hard-dock, but the Soyuz starts to fly away.
Issue#025

Reproduced that one. Sometimes it works, sometimes it doesn't. Probably frame-rate dependant, will try to find a workaround. -> fixed, tbc

---------- Post added at 11:15 PM ---------- Previous post was at 10:25 PM ----------

I modified the lift & moment coefficients and got better results, sticking at 0.4 of L/D :

BTW, that "reentry" didn't exceed 1.8G, which I find a little weird (why don't they do that in the real life ?), also as a consequence the landing zone was overshot by 3500 kilometers :

Code:
Orbiter Flight Data Log Record
==============================
Columns:
	TIME:     simulation time (seconds)
	ALT:      altitude (km)
	AIRSPEED: airspeed (m/s)
	MACH:     Mach number
	TEMP:     freestream temperature (K)
	STP:      static pressure (kPa)
	DNP:      dynamic pressure (kPa)
	AOA:      angle of attack (deg)
	SLIP:     horizontal slip angle (deg)
	LIFT:     total lift force (kN)
	DRAG:     total drag force (kN)
	L/D:      lift/drag ratio
	MASS:     vessel mass (kg)

# Log started for Soyuz-12
# ____TIME _______ALT __MACH ____AOA ___SLIP _____L/D
    225.45    68.8705  25.09  -179.5  -178.4   -0.011
    226.45    68.7383  25.07  -179.9  -178.5   -0.001
    227.46    68.6066  25.04   179.5  -178.7    0.010
    228.46    68.4736  25.01   179.2  -178.8    0.016
    229.47    68.3411  24.98   179.1  -179.0    0.019
    230.48    68.2082  24.95   179.1  -179.2    0.017
    231.48    68.0750  24.92   179.5  -179.4    0.011
    232.49    67.9419  24.89  -179.6  -179.7   -0.008
    233.49    67.8089  24.86  -177.9  -179.9   -0.042
    234.49    67.6755  24.83  -175.6   179.8   -0.088
    235.50    67.5433  24.80  -172.9   179.6   -0.143
    236.50    67.4100  24.76  -170.3   179.3   -0.194
    237.51    67.2777  24.73  -167.9   179.1   -0.244
    238.51    67.1459  24.70  -165.5   178.9   -0.292
    239.51    67.0152  24.67  -163.1   178.7   -0.339
    240.52    66.8852  24.64  -162.0   178.7   -0.360
    241.53    66.7556  24.61  -161.4   178.7   -0.373
    242.53    66.6278  24.58  -160.3   178.7   -0.394
    243.54    66.5010  24.55  -160.4   178.7   -0.393
    244.55    66.3746  24.52  -160.5   178.8   -0.391
    245.56    66.2509  24.49  -160.6   178.9   -0.390
    246.57    66.1280  24.46  -160.6   178.9   -0.388
    247.58    66.0057  24.43  -160.7   178.9   -0.387
    248.58    65.8856  24.40  -160.8   179.0   -0.385
    249.59    65.7664  24.36  -160.9   179.1   -0.383
    250.60    65.6481  24.33  -160.8   179.2   -0.384
    251.60    65.5322  24.30  -160.7   179.3   -0.387
    252.62    65.4173  24.27  -160.6   179.5   -0.389
    253.62    65.3031  24.24  -160.5   179.7   -0.391
    254.63    65.1912  24.21  -160.4   179.9   -0.393
    255.64    65.0805  24.18  -160.3  -179.9   -0.394
    256.65    64.9704  24.15  -160.2  -179.7   -0.396
    257.65    64.8628  24.12  -160.2  -179.5   -0.397
    258.67    64.7565  24.09  -160.2  -179.3   -0.397
    259.68    64.6509  24.06  -160.1  -179.2   -0.398
    260.68    64.5483  24.03  -160.1  -179.0   -0.398
    261.69    64.4466  24.00  -160.1  -179.0   -0.398
    262.70    64.3458  23.97  -160.2  -178.9   -0.397
    263.70    64.2476  23.94  -160.2  -178.9   -0.397
    264.71    64.1505  23.91  -160.2  -179.0   -0.396
    265.72    64.0545  23.88  -160.3  -179.0   -0.394
    266.72    63.9610  23.85  -160.4  -179.2   -0.393
    267.73    63.8687  23.82  -160.5  -179.3   -0.391
    268.74    63.7773  23.79  -160.6  -179.5   -0.389
    269.74    63.6885  23.76  -160.7  -179.7   -0.386
    270.75    63.6009  23.73  -160.9  -179.9   -0.383
    271.75    63.5150  23.70  -160.8   179.9   -0.384
    272.76    63.4312  23.68  -160.7   179.7   -0.387
    273.76    63.3478  23.65  -160.5   179.5   -0.390
    274.76    63.2670  23.62  -160.4   179.3   -0.392
    275.81    63.2017  23.59  -160.3   179.2   -0.394
    276.81    63.1066  23.56  -160.2   179.0   -0.396
    277.81    63.0310  23.53  -160.2   179.0   -0.397
    278.82    62.9559  23.50  -160.1   178.9   -0.398
    279.82    62.8832  23.47  -160.1   179.0   -0.398
    280.83    62.8120  23.44  -160.1   179.0   -0.398
    281.83    62.7427  23.42  -160.1   179.2   -0.398
    282.83    62.6755  23.39  -160.1   179.3   -0.398
    283.84    62.6088  23.36  -160.2   179.5   -0.397
    284.84    62.5445  23.33  -160.2   179.7   -0.396
    285.85    62.4818  23.30  -160.3   179.9   -0.395
    286.85    62.4209  23.28  -160.4  -179.9   -0.393
    287.85    62.3618  23.25  -160.5  -179.6   -0.391
    288.86    62.3034  23.22  -160.4  -179.4   -0.393
    289.87    62.2473  23.19  -160.2  -179.3   -0.395
    290.87    62.1930  23.17  -160.1  -179.1   -0.398
    291.87    62.1403  23.14  -160.0  -179.0   -0.400
    292.89    62.0890  23.11  -159.9  -179.0   -0.399
    293.90    62.0390  23.08  -159.9  -179.0   -0.398
    294.90    61.9914  23.06  -159.9  -179.0   -0.398
    295.90    61.9456  23.03  -159.9  -179.1   -0.399
    296.90    61.9013  23.00  -160.0  -179.3   -0.400
    297.91    61.8586  22.98  -160.1  -179.4   -0.398
    298.91    61.8176  22.95  -160.3  -179.6   -0.395
    299.92    61.7783  22.93  -160.4  -179.9   -0.392
    300.93    61.7400  22.90  -160.6   179.9   -0.389
    301.93    61.7037  22.87  -160.7   179.7   -0.386
    302.94    61.6690  22.85  -160.7   179.5   -0.387
    303.94    61.6358  22.82  -160.4   179.3   -0.392
    304.94    61.6042  22.80  -160.1   179.1   -0.398
    305.95    61.5741  22.77  -159.9   179.0   -0.398
    306.95    61.5457  22.75  -159.7   179.0   -0.395
    307.96    61.5185  22.72  -159.6   179.0   -0.393
    308.97    61.4930  22.70  -159.7   179.0   -0.394
    309.98    61.4689  22.67  -159.8   179.1   -0.397
    310.99    61.4465  22.65  -160.1   179.3   -0.399
    311.99    61.4256  22.62  -160.3   179.4   -0.394
    313.00    61.4061  22.60  -160.6   179.6   -0.389
    314.01    61.3880  22.58  -160.9   179.9   -0.383
    315.01    61.3714  22.55  -160.9  -179.9   -0.384
    316.01    61.3560  22.53  -160.9  -179.7   -0.383
    317.02    61.3420  22.51  -160.8  -179.5   -0.385
    318.03    61.3293  22.48  -160.4  -179.3   -0.392
    319.03    61.3180  22.46  -160.0  -179.1   -0.400
    320.04    61.3081  22.44  -160.0  -179.1   -0.400
    321.04    61.2995  22.41  -160.1  -179.2   -0.399
    322.04    61.2923  22.39  -160.1  -179.2   -0.399
    323.05    61.2863  22.37  -160.1  -179.2   -0.398
    324.05    61.2817  22.35  -160.1  -179.2   -0.398
    325.06    61.2784  22.33  -160.1  -179.2   -0.399
    326.07    61.2763  22.30  -160.0  -179.2   -0.399
    327.07    61.2754  22.28  -160.1  -179.2   -0.399
    328.08    61.2758  22.26  -160.1  -179.2   -0.398
    329.09    61.2774  22.24  -160.0  -179.2   -0.399
    330.10    61.2802  22.22  -160.1  -179.2   -0.399
    331.10    61.2841  22.20  -160.0  -179.2   -0.400
    332.11    61.2891  22.18  -160.1  -179.2   -0.399
    333.11    61.2953  22.16  -160.1  -179.2   -0.398
    334.12    61.3026  22.14  -160.2  -179.2   -0.396
    335.12    61.3108  22.12  -160.2  -179.2   -0.397
    336.13    61.3201  22.10  -159.9  -179.2   -0.399
    337.13    61.3304  22.08  -159.8  -179.2   -0.397
    338.14    61.3418  22.06  -159.9  -179.3   -0.399
    339.14    61.3540  22.04  -160.1  -179.3   -0.399
    340.14    61.3672  22.02  -160.2  -179.4   -0.396
    341.15    61.3813  22.00  -160.4  -179.5   -0.393
    342.16    61.3963  21.98  -160.5  -179.7   -0.390
    343.16    61.4119  21.96  -160.6  -179.9   -0.389
    344.17    61.4287  21.95  -160.4   180.0   -0.392
    345.17    61.4459  21.93  -160.2   179.8   -0.396
    346.18    61.4641  21.91  -160.0   179.6   -0.399
    347.19    61.4831  21.89  -159.9   179.5   -0.398
    348.19    61.5027  21.87  -159.8   179.4   -0.396
    349.21    61.5231  21.86  -159.7   179.3   -0.396
    350.21    61.5443  21.84  -159.8   179.2   -0.397
    351.22    61.5659  21.82  -159.9   179.2   -0.399
    352.23    61.5883  21.80  -160.1   179.2   -0.399
    353.24    61.6114  21.79  -160.0   179.3   -0.400
    354.24    61.6349  21.77  -159.8   179.4   -0.396
    355.25    61.6589  21.75  -159.6   179.5   -0.394
    356.26    61.6837  21.74  -159.6   179.6   -0.393
    357.26    61.7088  21.72  -159.7   179.8   -0.395
    358.27    61.7344  21.71  -159.9   179.9   -0.399
    359.28    61.7606  21.69  -160.2  -179.9   -0.397
    360.29    61.7870  21.67  -160.4  -179.7   -0.392
    361.30    61.8138  21.66  -160.7  -179.6   -0.387
    362.31    61.8412  21.64  -160.7  -179.4   -0.387
    363.31    61.8686  21.63  -160.6  -179.3   -0.389
    364.32    61.8963  21.61  -160.5  -179.3   -0.391
    365.33    61.9245  21.60  -160.4  -179.2   -0.393
    366.34    61.9528  21.58  -160.3  -179.2   -0.394
    367.34    61.9810  21.57  -160.1  -179.2   -0.399
    368.35    62.0099  21.55  -160.0  -179.2   -0.399
    369.35    62.0388  21.54  -160.1  -179.3   -0.398
    370.36    62.0679  21.52  -160.2  -179.3   -0.396
    371.37    62.0973  21.51  -160.3  -179.4   -0.394
    372.37    62.1265  21.49  -160.4  -179.5   -0.392
    373.39    62.1561  21.48  -160.6  -179.7   -0.389
    374.40    62.1858  21.47  -160.7  -179.8   -0.386
    375.40    62.2151  21.45  -160.9   180.0   -0.383
    376.41    62.2446  21.44  -161.0   179.8   -0.381
    377.42    62.2742  21.42  -160.7   179.7   -0.387
    378.43    62.3034  21.41  -160.2   179.5   -0.397
    379.43    62.3326  21.40  -160.2   179.5   -0.397
    380.44    62.3618  21.38  -160.3   179.6   -0.395
    381.44    62.3907  21.37  -160.4   179.6   -0.393
    382.45    62.4197  21.36  -160.3   179.7   -0.394
    383.45    62.4484  21.34  -160.1   179.7   -0.398
    384.46    62.4769  21.33  -160.0   179.8   -0.400
    385.46    62.5056  21.32  -160.0   179.8   -0.400
    386.47    62.5339  21.30  -160.1   179.8   -0.398
    387.48    62.5620  21.29  -160.2   179.8   -0.396
    388.49    62.5901  21.28  -160.3   179.8   -0.394
    389.49    62.6175  21.26  -160.4   179.9   -0.392
    390.50    62.6448  21.25  -160.6   179.9   -0.389
    391.51    62.6719  21.24  -160.7   179.9   -0.386
    392.51    62.6984  21.22  -160.5   180.0   -0.391
    393.52    62.7246  21.21  -160.2  -180.0   -0.396
    394.53    62.7506  21.20  -160.0  -179.9   -0.400
    395.53    62.7760  21.18  -159.8  -179.9   -0.396
    396.54    62.8011  21.17  -159.6  -179.9   -0.393
    397.54    62.8256  21.16  -159.6  -179.8   -0.392
    398.55    62.8498  21.15  -159.6  -179.8   -0.393
    399.55    62.8735  21.13  -159.8  -179.8   -0.396
    400.56    62.8964  21.12  -160.0  -179.8   -0.400
    401.56    62.9192  21.11  -160.2  -179.8   -0.396
    402.56    62.9414  21.10  -160.5  -179.8   -0.391
    403.57    62.9630  21.08  -160.7  -179.8   -0.386
    404.58    62.9842  21.07  -161.0  -179.8   -0.380
    405.58    63.0045  21.06  -161.2  -179.8   -0.376
    406.59    63.0243  21.04  -161.3  -179.8   -0.375
    407.60    63.0434  21.03  -161.4  -179.8   -0.373
    408.61    63.0617  21.02  -161.5  -179.9   -0.370
    409.61    63.0791  21.01  -161.3  -179.9   -0.375
    410.62    63.0960  20.99  -160.6  -179.9   -0.389
    411.62    63.1120  20.98  -160.4  -179.9   -0.392
    412.63    63.1273  20.97  -160.1  -179.9   -0.399
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# Log stopped for Soyuz-12
 
Last edited:

Urwumpe

Not funny anymore
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What is your drag coefficient and area now?
 

N_Molson

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Here is the aerodynamic function in the current state :

Code:
void VLiftCoeff (double aoa, double M, double Re, double *cl, double *cm, double *cd)
{
	int i;
	const int nabsc = 19;
	// Angle of attack                   -180,     -160,     -140,     -120,     -100,     -80,     -60,     -40,      -20,     0,      20,      40,      60,      80,     100,     120,     140,     160,     180,
	static const double AOA[nabsc]= {-180*RAD, -160*RAD, -140*RAD, -120*RAD, -100*RAD, -80*RAD, -60*RAD, -40*RAD,  -20*RAD, 0*RAD,  20*RAD,  40*RAD,  60*RAD,  80*RAD, 100*RAD, 120*RAD, 140*RAD, 160*RAD, 180*RAD};
	static const double CL[nabsc] = {       0,    -0.172,    -0.011,        0,        0,       0,       0,       0,        0,     0,       0,       0,       0,       0,       0,       0,   +0.011,  +0.172,       0};
	static const double CM[nabsc] = {-0.00014,  -0.00037,   -0.001,   -0.005,    -0.006,   -0.006,  -0.005, -0.003,  -0.002,     0, +0.002, +0.003, +0.005, +0.006, +0.006, +0.005, +0.001, +0.00037, +0.00014};

	for (i = 0; i < nabsc-1 && AOA[i+1] < aoa; i++);
	double f = (aoa-AOA[i]) / (AOA[i+1]-AOA[i]);
	*cl = CL[i] + (CL[i+1]-CL[i]) * f;  // aoa-dependent lift coefficient
	*cm = CM[i] + (CM[i+1]-CM[i]) * f;  // aoa-dependent moment coefficient
	double saoa = sin(aoa);
	double pd = 0.21 + 0.01*saoa*saoa;  // profile drag
	*cd = pd + oapiGetInducedDrag (*cl, 6.82, 0.4);
	// profile drag + (lift-)induced drag
};
// 2. horizontal lift component (vertical stabiliser and body)
void HLiftCoeff (double beta, double M, double Re, double *cl, double *cm, double *cd)
{
	int i;
	const int nabsc = 19;
	static const double BETA[nabsc] = {-180*RAD, -160*RAD, -140*RAD, -120*RAD, -100*RAD, -80*RAD, -60*RAD, -40*RAD,  -20*RAD, 0*RAD,  20*RAD,  40*RAD,  60*RAD,  80*RAD, 100*RAD, 120*RAD, 140*RAD, 160*RAD, 180*RAD};
	static const double CL[nabsc]   = {       0,    -0.15,    -0.05,        0,        0,       0,       0,       0,        0,     0,       0,       0,       0,       0,       0,       0,    0.05,    0.15,       0};
	for (i = 0; i < nabsc-1 && BETA[i+1] < beta; i++);
	*cl = CL[i] + (CL[i+1]-CL[i]) * (beta-BETA[i]) / (BETA[i+1]-BETA[i]);
	*cm = 0;
	*cd = 0.21 + oapiGetInducedDrag (*cl, 6.82, 0.04);
};

The capsule is defined as a sort of "+ wing" :

CreateAirfoil (LIFT_VERTICAL, _V(0, 0,0.01), VLiftCoeff, 2.17, 6.82, 0.1);
CreateAirfoil (LIFT_HORIZONTAL, _V(0, 0,0.001), HLiftCoeff, 2.17, 6.82, 0.1);
 

N_Molson

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The aft engines also seem to be angled inward a lot:

Issue #026

Fixed, I assumed a 45° inward angle (correct me if you have the precise value), and the RCS handles MUCH better in DPO mode.
 

Urwumpe

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Issue #026

Fixed, I assumed a 45° inward angle (correct me if you have the precise value), and the RCS handles MUCH better in DPO mode.

I had either 45° or 30° depending on how I try to reconstruct the nozzles, but 45° really has the better probability. Can't wait to test it. :)
 

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EDIT: I notice that the DPO is firing effectively pro and retrograde at the same time without me commanding it... did you implement some docking guidance without IGLA, with too tight deadbands?

Issue #027

Fixed, the CG was moved back so that most unwanted torque in translation mode got eliminated. Also, the deadband was slightly enlarged, avoiding the system to "lock" and spill H2O2 in all directions.
 

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Issue #027

Fixed, the CG was moved back so that most unwanted torque in translation mode got eliminated. Also, the deadband was slightly enlarged, avoiding the system to "lock" and spill H2O2 in all directions.

couldn't this be perfectly handled by having both gyroscopes active and controlling the attitude?
 

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couldn't this be perfectly handled by having both gyroscopes active and controlling the attitude?

Ah, you mean using an absolute reference point in space at which the nose is pointing as an instant t instead of relying on angular velocity ? I still have trouble with this ; as you may have noticed, the "uncage gyros" thing doesn't work very well in its current state (the Global2Local & co functions are driving me crazy, and I know nothing at vectors, so I'm completely lost with trigonometric calculations, dot products, rotation matrixes, mul and tmul operators). But I'll search further in that way.
 

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Ah, you mean using an absolute reference point in space at which the nose is pointing as an instant t instead of relying on angular velocity ? I still have trouble with this ; as you may have noticed, the "uncage gyros" thing doesn't work very well in its current state (the Global2Local & co functions are driving me crazy, and I know nothing at vectors, so I'm completely lost with trigonometric calculations, dot products, rotation matrixes, mul and tmul operators). But I'll search further in that way.

Well, global2Local is the wrong function there, you should try GlobalRot or use the transformation matrix directly.

You can for example use globalrot for transforming unit vectors from local to global and use these vectors then for calculating the angular errors between your current attitude and the planned attitude.
 

N_Molson

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Well, global2Local is the wrong function there, you should try GlobalRot or use the transformation matrix directly.

Well, in fact it's what I tried. Any suggestions on what is going wrong here ?

Code:
	if (gyro_uncage == 1)
	{
		VECTOR3 lvpos = {0,0,1};
		GetGlobalOrientation(lvpos);

		MATRIX3 R3;
		vs->GetRotationMatrix(R3);						//get rotation matrix
		lvpos = tmul(R3,lvpos);

		double abs_Pitch = lvpos.x*DEG;
		double abs_Yaw = lvpos.y*DEG;

		if (done08 == 0)
		{
			abs_Pitch_m = lvpos.x*DEG;
			abs_Yaw_m = lvpos.y*DEG;
			done08 = 1;
		}

		double X_diff = abs_Pitch_m - abs_Pitch;
		double Y_diff = abs_Yaw_m - abs_Yaw;

                ...
         }

abs_pitch = "absolute", or "reference" pitch (the point in space at which the nose is pointing at an instant t we want to keep as a reference)
abs_yaw = ... yaw
 
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