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LD-10 vs SD-10 | DCS OB 2.7.16.28157 | DSplayer

Created 3 years agoDiff never expires

Lines
Total	38
Removed	-23.7%9

Words
Total	355
Removed	-4.5%16

38 lines

Lines
Total	39
Added	+25.6%10

Words
Total	456
Added	+25.7%117

39 lines

LD_10_ARM.fm = {

fm = {

mass = ld10_mass,

mass = sd10_mass,

caliber = 0.203,

wind_sigma = 0.0,

wind_time = 0.0,

tail_first = 1,

tail_first = 0,

fins_part_val = 0,

rotated_fins_inp = 0,

delta_max = math.rad(20),

draw_fins_conv = {math.rad(90),1,1},

L = 0.203,

S = 0.0324,

Ix = 1.5,

Iy = 190,

Iz = 190,

Mxd = 0.1 * 57.3,

Mxw = -15.8,

table_scale = 0.2,

table_degree_values = 1,

-- Mach | 0.0 0.2 0.4 0.6 0.8 1.0 1.2 1.4 1.6 1.8 2.0 2.2 2.4 2.6 2.8 3.0 3.2 3.4 3.6 3.8 4.0 |

-- Mach | 0.0 0.2 0.4 0.6 0.8 1.0 1.2 1.4 1.6 1.8 2.0 2.2 2.4 2.6 2.8 3.0 3.2 3.4 3.6 3.8 4.0 4.2 4.4 4.6 4.8 5.0 |

Cx0 = { 0.4727, 0.4727, 0.4727, 0.4727, 0.4838, 0.7609, 0.8869, 0.86198, 0.81793, 0.76899, 0.72481, 0.68476, 0.64836, 0.61529, 0.58515, 0.55744, 0.53195, 0.50829, 0.48624, 0.46561, 0.4461, 0.42772, 0.41035, 0.3941, 0.37898, 0.366 },

CxB = { 0.021, 0.021, 0.021, 0.021, 0.021, 0.138, 0.153, 0.146, 0.1382, 0.1272, 0.1167, 0.1073, 0.0987, 0.0909, 0.0837, 0.077, 0.0708, 0.065, 0.0595, 0.0544, 0.0495, 0.0449, 0.0406, 0.0364, 0.0324, 0.0286 },

K1 = { 0.00264, 0.00264, 0.00264, 0.00264, 0.00264, 0.00264, 0.0022, 0.001873, 0.0016435, 0.0014752, 0.0013448, 0.0012436, 0.0011534, 0.0010742, 0.0010149, 0.0009484, 0.0009016, 0.0008476, 0.000795, 0.0007529, 0.0007122, 0.0006727, 0.0006343, 0.0006058, 0.0005781, 0.00056 },

K2 = { -0.00257, -0.00257, -0.00257, -0.00257, -0.00257, -0.00265, -0.002274, -0.002034, -0.0018241, -0.0016225, -0.0014468, -0.001275, -0.0011248, -0.0009777, -0.0008514, -0.0007274, -0.0006236, -0.0005217, -0.0004393, -0.0003584, -0.0002968, -0.0002363, -0.0001949, -0.0001546, -0.0001335, -0.000114 },

Cya = { 0.3207, 0.3207, 0.3207, 0.3207, 0.3381, 0.4226, 0.4651, 0.5049, 0.5175, 0.5033, 0.4919, 0.4815, 0.4729, 0.4653, 0.4586, 0.4528, 0.4479, 0.444, 0.441, 0.4371, 0.4341, 0.4321, 0.43, 0.4271, 0.426, 0.424 },

Cza = { 0.3207, 0.3207, 0.3207, 0.3207, 0.3381, 0.4226, 0.4651, 0.5049, 0.5175, 0.5033, 0.4919, 0.4815, 0.4729, 0.4653, 0.4586, 0.4528, 0.4479, 0.444, 0.441, 0.4371, 0.4341, 0.4321, 0.43, 0.4271, 0.426, 0.424 },

Mya = { -0.7724, -0.7724, -0.7724, -0.7724, -0.8442, -1.0226, -0.9581, -0.85133, -0.7413, -0.59726, -0.49729, -0.42745, -0.37784, -0.3414, -0.31341, -0.29077, -0.27141, -0.25428, -0.23854, -0.22399, -0.21035, -0.19771, -0.18616, -0.1758, -0.16696, -0.16075 },

Mza = { -0.7724, -0.7724, -0.7724, -0.7724, -0.8442, -1.0226, -0.9581, -0.85133, -0.7413, -0.59726, -0.49729, -0.42745, -0.37784, -0.3414, -0.31341, -0.29077, -0.27141, -0.25428, -0.23854, -0.22399, -0.21035, -0.19771, -0.18616, -0.1758, -0.16696, -0.16075 },

Myw = { -2.0, -2.0},

Myw = { -9.55874, -9.55874, -9.55874, -9.55874, -9.81248, -12.17459, -10.86314, -10.80419, -10.7503, -10.67431, -10.57881, -10.46632, -10.33913, -10.19945, -10.04929, -9.89055, -9.72493, -9.55397, -9.37918, -9.20172, -9.02292, -8.84372, -8.66508, -8.48791, -8.31347, -8.14394 },

Mzw = { -2.0, -2.0},

Mzw = { -9.55874, -9.55874, -9.55874, -9.55874, -9.81248, -12.17459, -10.86314, -10.80419, -10.7503, -10.67431, -10.57881, -10.46632, -10.33913, -10.19945, -10.04929, -9.89055, -9.72493, -9.55397, -9.37918, -9.20172, -9.02292, -8.84372, -8.66508, -8.48791, -8.31347, -8.14394 },

A1trim = { 4.0, 6.0, 10.0, 15.0},

A1trim = { 27.6, 27.6, 27.6, 27.6, 27.55, 30.38, 31.982, 32.774, 33.234, 33.561, 33.829, 34.07, 34.286, 34.491, 34.687, 34.875, 35.056, 35.232, 35.401, 35.564, 35.721, 35.871, 36.015, 36.151, 36.279, 36.4 },

A2trim = { 4.0, 6.0, 10.0, 15.0},

A2trim = { 27.6, 27.6, 27.6, 27.6, 27.55, 30.38, 31.982, 32.774, 33.234, 33.561, 33.829, 34.07, 34.286, 34.491, 34.687, 34.875, 35.056, 35.232, 35.401, 35.564, 35.721, 35.871, 36.015, 36.151, 36.279, 36.4 },

model_roll = math.rad(45),

fins_stall = 1,

}

Diff salvati

Testo originale

Apri file

LD_10_ARM.fm = {
        mass                = ld10_mass,
        caliber             = 0.203,
        wind_sigma          = 0.0,
        wind_time           = 0.0,
        tail_first          = 1,
        fins_part_val       = 0,
        rotated_fins_inp    = 0,
        delta_max           = math.rad(20),
        draw_fins_conv      = {math.rad(90),1,1},
        L                   = 0.203,
        S                   = 0.0324,
        Ix                  = 1.5,
        Iy                  = 190,
        Iz                  = 190,

Mxd                 = 0.1 * 57.3,
        Mxw                 = -15.8,

table_scale         = 0.2,
        table_degree_values = 1,
        --    Mach      | 0.0        0.2        0.4        0.6        0.8        1.0        1.2        1.4        1.6        1.8        2.0        2.2        2.4        2.6        2.8        3.0        3.2        3.4        3.6        3.8        4.0     |
        Cx0 = {    0.4727,    0.4727,    0.4727,    0.4727,    0.4838,    0.7609,     0.8869,     0.86198,    0.81793,     0.76899,     0.72481,     0.68476,    0.64836,    0.61529,    0.58515,    0.55744,    0.53195,    0.50829,    0.48624,    0.46561,    0.4461,     0.42772,    0.41035,    0.3941,     0.37898,    0.366    },
        CxB = {    0.021,     0.021,     0.021,     0.021,     0.021,     0.138,      0.153,      0.146,      0.1382,      0.1272,      0.1167,      0.1073,     0.0987,     0.0909,     0.0837,     0.077,      0.0708,     0.065,      0.0595,     0.0544,     0.0495,     0.0449,     0.0406,     0.0364,     0.0324,     0.0286    },
        K1  = {    0.00264,   0.00264,   0.00264,   0.00264,   0.00264,   0.00264,    0.0022,     0.001873,   0.0016435,   0.0014752,   0.0013448,   0.0012436,  0.0011534,  0.0010742,  0.0010149,  0.0009484,  0.0009016,  0.0008476,  0.000795,   0.0007529,  0.0007122,  0.0006727,  0.0006343,  0.0006058,  0.0005781,  0.00056    },
        K2  = {    -0.00257,  -0.00257,  -0.00257,  -0.00257,  -0.00257,  -0.00265,   -0.002274,  -0.002034,  -0.0018241,  -0.0016225,  -0.0014468,  -0.001275,  -0.0011248, -0.0009777, -0.0008514, -0.0007274, -0.0006236, -0.0005217, -0.0004393, -0.0003584, -0.0002968, -0.0002363, -0.0001949, -0.0001546, -0.0001335, -0.000114    },
        Cya = {    0.3207,    0.3207,    0.3207,    0.3207,    0.3381,    0.4226,     0.4651,     0.5049,     0.5175,      0.5033,      0.4919,      0.4815,     0.4729,     0.4653,     0.4586,     0.4528,     0.4479,     0.444,      0.441,      0.4371,     0.4341,     0.4321,     0.43,       0.4271,     0.426,      0.424    },
        Cza = {    0.3207,    0.3207,    0.3207,    0.3207,    0.3381,    0.4226,     0.4651,     0.5049,     0.5175,      0.5033,      0.4919,      0.4815,     0.4729,     0.4653,     0.4586,     0.4528,     0.4479,     0.444,      0.441,      0.4371,     0.4341,     0.4321,     0.43,       0.4271,     0.426,      0.424    },
        Mya = {    -0.7724,   -0.7724,   -0.7724,   -0.7724,   -0.8442,   -1.0226,    -0.9581,    -0.85133,   -0.7413,     -0.59726,    -0.49729,    -0.42745,   -0.37784,   -0.3414,    -0.31341,   -0.29077,   -0.27141,   -0.25428,   -0.23854,   -0.22399,   -0.21035,   -0.19771,   -0.18616,   -0.1758,    -0.16696,   -0.16075    },
        Mza = {    -0.7724,   -0.7724,   -0.7724,   -0.7724,   -0.8442,   -1.0226,    -0.9581,    -0.85133,   -0.7413,     -0.59726,    -0.49729,    -0.42745,   -0.37784,   -0.3414,    -0.31341,   -0.29077,   -0.27141,   -0.25428,   -0.23854,   -0.22399,   -0.21035,   -0.19771,   -0.18616,   -0.1758,    -0.16696,   -0.16075    },
        Myw = {    -2.0,    -2.0},
        Mzw = {    -2.0,    -2.0},
        A1trim = { 4.0, 6.0, 10.0, 15.0},
        A2trim = { 4.0, 6.0, 10.0, 15.0},

model_roll = math.rad(45),
        fins_stall = 1,
    }

Testo modificato

Apri file

fm = {
        mass                = sd10_mass,
        caliber             = 0.203,
        wind_sigma          = 0.0,
        wind_time           = 0.0,
        tail_first          = 0,
        fins_part_val       = 0,
        rotated_fins_inp    = 0,
        delta_max           = math.rad(20),
        draw_fins_conv      = {math.rad(90),1,1},
        L                   = 0.203,
        S                   = 0.0324,
        Ix                  = 1.5,
        Iy                  = 190,
        Iz                  = 190,

Mxd                 = 0.1 * 57.3,
        Mxw                 = -15.8,

table_scale         = 0.2,
        table_degree_values = 1,
        -- Mach   | 0.0        0.2        0.4        0.6        0.8         1.0        1.2         1.4         1.6          1.8          2.0          2.2         2.4         2.6         2.8         3.0         3.2         3.4         3.6         3.8         4.0         4.2         4.4         4.6         4.8         5.0 |
        Cx0 = {    0.4727,    0.4727,    0.4727,    0.4727,    0.4838,    0.7609,     0.8869,     0.86198,    0.81793,     0.76899,     0.72481,     0.68476,    0.64836,    0.61529,    0.58515,    0.55744,    0.53195,    0.50829,    0.48624,    0.46561,    0.4461,     0.42772,    0.41035,    0.3941,     0.37898,    0.366    },
        CxB = {    0.021,     0.021,     0.021,     0.021,     0.021,     0.138,      0.153,      0.146,      0.1382,      0.1272,      0.1167,      0.1073,     0.0987,     0.0909,     0.0837,     0.077,      0.0708,     0.065,      0.0595,     0.0544,     0.0495,     0.0449,     0.0406,     0.0364,     0.0324,     0.0286    },
        K1  = {    0.00264,   0.00264,   0.00264,   0.00264,   0.00264,   0.00264,    0.0022,     0.001873,   0.0016435,   0.0014752,   0.0013448,   0.0012436,  0.0011534,  0.0010742,  0.0010149,  0.0009484,  0.0009016,  0.0008476,  0.000795,   0.0007529,  0.0007122,  0.0006727,  0.0006343,  0.0006058,  0.0005781,  0.00056    },
        K2  = {    -0.00257,  -0.00257,  -0.00257,  -0.00257,  -0.00257,  -0.00265,   -0.002274,  -0.002034,  -0.0018241,  -0.0016225,  -0.0014468,  -0.001275,  -0.0011248, -0.0009777, -0.0008514, -0.0007274, -0.0006236, -0.0005217, -0.0004393, -0.0003584, -0.0002968, -0.0002363, -0.0001949, -0.0001546, -0.0001335, -0.000114    },
        Cya = {    0.3207,    0.3207,    0.3207,    0.3207,    0.3381,    0.4226,     0.4651,     0.5049,     0.5175,      0.5033,      0.4919,      0.4815,     0.4729,     0.4653,     0.4586,     0.4528,     0.4479,     0.444,      0.441,      0.4371,     0.4341,     0.4321,     0.43,       0.4271,     0.426,      0.424    },
        Cza = {    0.3207,    0.3207,    0.3207,    0.3207,    0.3381,    0.4226,     0.4651,     0.5049,     0.5175,      0.5033,      0.4919,      0.4815,     0.4729,     0.4653,     0.4586,     0.4528,     0.4479,     0.444,      0.441,      0.4371,     0.4341,     0.4321,     0.43,       0.4271,     0.426,      0.424    },
        Mya = {    -0.7724,   -0.7724,   -0.7724,   -0.7724,   -0.8442,   -1.0226,    -0.9581,    -0.85133,   -0.7413,     -0.59726,    -0.49729,    -0.42745,   -0.37784,   -0.3414,    -0.31341,   -0.29077,   -0.27141,   -0.25428,   -0.23854,   -0.22399,   -0.21035,   -0.19771,   -0.18616,   -0.1758,    -0.16696,   -0.16075    },
        Mza = {    -0.7724,   -0.7724,   -0.7724,   -0.7724,   -0.8442,   -1.0226,    -0.9581,    -0.85133,   -0.7413,     -0.59726,    -0.49729,    -0.42745,   -0.37784,   -0.3414,    -0.31341,   -0.29077,   -0.27141,   -0.25428,   -0.23854,   -0.22399,   -0.21035,   -0.19771,   -0.18616,   -0.1758,    -0.16696,   -0.16075    },
        Myw = {    -9.55874,  -9.55874,  -9.55874,  -9.55874,  -9.81248,  -12.17459,  -10.86314,  -10.80419,  -10.7503,    -10.67431,   -10.57881,   -10.46632,  -10.33913,  -10.19945,  -10.04929,  -9.89055,   -9.72493,   -9.55397,   -9.37918,   -9.20172,   -9.02292,   -8.84372,   -8.66508,   -8.48791,   -8.31347,   -8.14394    },
        Mzw = {    -9.55874,  -9.55874,  -9.55874,  -9.55874,  -9.81248,  -12.17459,  -10.86314,  -10.80419,  -10.7503,    -10.67431,   -10.57881,   -10.46632,  -10.33913,  -10.19945,  -10.04929,  -9.89055,   -9.72493,   -9.55397,   -9.37918,   -9.20172,   -9.02292,   -8.84372,   -8.66508,   -8.48791,   -8.31347,   -8.14394    },
        A1trim = { 27.6,      27.6,      27.6,      27.6,      27.55,     30.38,      31.982,     32.774,     33.234,      33.561,      33.829,      34.07,      34.286,     34.491,     34.687,     34.875,     35.056,     35.232,     35.401,     35.564,     35.721,     35.871,     36.015,     36.151,     36.279,     36.4    },
        A2trim = { 27.6,      27.6,      27.6,      27.6,      27.55,     30.38,      31.982,     32.774,     33.234,      33.561,      33.829,      34.07,      34.286,     34.491,     34.687,     34.875,     35.056,     35.232,     35.401,     35.564,     35.721,     35.871,     36.015,     36.151,     36.279,     36.4    },

model_roll = math.rad(45),
        fins_stall = 1,
    },