tractor 802
TRANSCRIPT
k2 - k1 = 0.88S = 16.26 i w_f i_f delta_xc = 1.48 1 0.5945 0.15708 0.278
anpha_ow 0.017453 2 0.882 0.15708 1.13 1.036 0 0.6844 1.07 0 1.9725 0.943 0 0.536 0.528 -0.05236 3.5927 0.1205 -0.05236 0.684
C_Mof =
1 0.5945 1.25 0.2782 0.882 1.4 1.13 1.036 3 0.6845 0.943 0.0359 0.536 0.528 0.315 3.5927 0.1205 0.6045 0.684
C_Manphaf =
0.0171480.1493510.0128130.0394050.008226
-0.034955-0.0003470.1916410.000192
0.1228171.1980032.202403
0.016920.3154390.0060043.8615850.004396
m_empty = Rx = Ry = Rz = M = Ixx = Iyy = Izz =0
5000
10000
15000
20000
25000
30000
Column E
bw = 18.06 Wing Airfoil NACA 4415 Cau 1 Cau 2Sw = 37.25 Tail Airfoil NACA 0012 Cmow = -0.12321 alpha_trim_pitch = 2.41ARw = 8.8 Cmalphaw = -0.24621iw = 2 Clalpha_t = 6.3651 Cau 3CLow = 0.4642 CLalpha_t = 4.6851 Cmot = 0.194358 CLdelta_e = 0.6237Clalpha_w = 5.9914 Cmalphat = -1.455651 CMdelta_e = -1.741CLalpha_w = 4.9242 c_mean = 2.06 xNP/c = 0.54m = 7257 VH = 0.4826 Cmof = 0.00019e = 0.8 epsilon_o = 0.0336 Cmalphaf = 0.0044 Cau 4
xichma = 0.7861 d_epsilon = 0.3562 CLo = 0.3946bt = 6.03 Cmo = 0.0713 CLalpha = 5.4457St = 6.44 Vcruise = 300 83.33333333 Cmalpha = -1.6975 CL_cruise = 0.5713bf = 1.425 CL_trim = 0.1767Sf = 2.81 QSw = 124551.1306 delta_e_trim = 0.0105Sa = 4.61 QSw/m = 17.16289522 alpha_trim = 0.0312Se = 3 Elevator Down Sr = 1.57 m_empty = 2951lt = 5.75 Rx = 0.248 Cau 5lv = 6.1 Ry = 0.338 CD_alpha = 0.3355 CD_cruise = 0.0542lf = 10.95 Rz = 0.393 (L/D)cruise = 10.54it = -1 M = 14.505 0.171189 Cxu = -0.1626ARt = 5.65 Ixx = 14774.1346 0.342378xCG/c = 0.2 Iyy = 10088.4591 5.44567 Cau 6Cmacw = -0.1 Izz = 23932.2629 0.02477 Czu = -1.1426swept_angle = 0 -0.005927zw = 0.18 nu_d_beta = 0.9486 0.374253d = 2.4 CLalpha_f = 1.6734 3.937643
ARf = 0.722642 Cybeta_tail = -0.1262 3.983754 0.871202285121dihedral = 3 Vv = 0.2234 -0.001088 1.376785250584zv = -1.46 lamda_w = 0.701 0.068725 6.777682420151
to_a = 0.35 -0.036915 0.402985074627y1 = 4.515 0.398843930636y2 = 9.03 5.974539451752c_root = 1.63 -0.0547519 0.739807842119K = -0.12 1.051155544015Clbeta_diheral = -0.00025 1.371072448715delta_Clbeta = 0.0002 2.693586081537
0.365935919056
Cxu = -0.1626 Xu = -0.0335Cxalpha = 0.29 Xalpha = 4.9772Czu = -1.1426 Zu = -0.2353Czalpha = -5.4999 Zalpha = -94.3942 Delta_Z = -1219.236Czalpha_point = -1.6108 Zalpha_point = -0.3417Czq = -4.5221 Zq = -0.9593Czdelta_e = -0.6237 Zdelta_e = -10.7045Cmu = 0 Mu = 0Cmalpha = -1.6975 Malpha = -43.1718
Cmalpha_point = -4.496 Malpha_point = -1.4133Cmq = -12.6223 Mq = -3.9678
ACmdelta_e = -1.741 Mdelta_e = -44.2781Cybeta = -0.1197 Xw = 0.0486
0.601606 Cyp = 0 Zw = -1.13271.787628 Cyr = 0.0853 Zw_point = -0.0041
Elevator Down Cydelta_r = 0.0972 Mw = -0.5181Cnbeta = 0.3546 Mw_point = -0.017Cnp = -0.0714 Ybeta = -2.0544Cnr = -0.2525 Yp = 0Cldelta_a = -0.1571 Yr = 0.1586Cndelta_a = -0.0215 Ydelta_a = 0Cndelta_r = -0.2879 Ydelta_r = 1.6682Clbeta = -0.0428 Nbeta = 33.3289Clp = -0.8278 Np = -1.178Clr = 0.1359 Nr = -4.1658Cldelta_r = -0.0231 Ndelta_a = -2.0208
Ndelta_r = -27.0597
Shortperiodmode
Phugoidmode
Lbeta = -6.5164Lp = -13.6571Lr = 2.2421Ldelta_a = -23.9188Ldelta_r = -3.517
p1 =p2 =z1_alpha =k1 =
k1 =
Deltaalpha
Pure pitching motionomega_1 = 6.5705fn = 0.954Period_n = 1.0482damping ratio = 0.4095xichma_1 = -2.69062omega_n = 5.994334
Longitudinal motion Lateral - Directional motiont_long t_shot
-0.0335 0.0486 0 -9.806
A
-0.0247 0 -0.9981 0.1177 0 0-0.2353 -1.1327 83.33333 0 -6.5164 -13.6571 2.2421 0 0.5 0.1
0.004 -0.4988 -5.384467 0 33.3289 -1.178 -4.1658 0 1 0.20 0 1 0 0 1 0 0 1.5 0.3
xichma_1_sp = -3.516 xichma_1 = -7.1403 2 0.4omega_n_sp = 4.7417 omega_n = 0.9203 2.5 0.5fn_sp = 0.7547 fn = 0.1465 3 0.6Period_n_sp = 1.325 Period = 6.8259 3.5 0.7omega_1_sp = 5.903 omega_1 = 7.1994 4 0.8damping ratio_sp = 0.5956 damping ratio = 0.9918 4.5 0.9xichma_1_ph = -0.0267 Roll mode -14.9943 5 1omega_n_ph = 0.1929 Spiral -0.0054 5.5 1.1fn_ph = 0.0307 6 1.2Period_n_ph = 32.5733 Delta_r = 5 6.5 1.3omega_1_ph = 0.1947 Delta_Ki_trim = -4.0595 7 1.4damping ratio_ph = 0.1371 Phi = 0.1282 7.5 1.5
8 1.6
DutchRoll
mode
Approximation Short period 8.5 1.7omega_1_sp = 6.9041 error = -0.1696 9 1.8damping ratio_sp = 0.4717 error = 0.208 9.5 1.9xichma_1_sp = -3.2567 10 2omega_n_sp = 6.0878 10.5 2.1fn_sp = 0.9689 11 2.2Period_sp = 1.0321 11.5 2.3
12 2.4Short Period Mode Long Period Mode 12.5 2.5
A_alpha = -0.128454 A_theta = 0.128454 13 2.6B_alpha = -44.78778 B_theta = -0.0259220172 13.5 2.7A = 1 A = 1 14 2.8B = 6.51383 B = 0.0335 -0.193873 14.5 2.9C = 47.66625 C = 0.0276882216 0.44031 15 3K_alpha = -0.128454 K_theta = 0.128454 0.0276 15.5 3.1B/A = 6.51383 z1_theta = 0.2018 0.220155 16 3.2C/A = 47.66625 B/A = 0.0335 16.5 3.3Delta = -148.235 C/A = 0.0276882216 17 3.4sqrt(Delta) = 12.17518 Delta = -0.1096306364 17.5 3.5
-3.2569152 6.08759 j sqrt(Delta) = 0.33110517423 18 3.6-3.2569152 -6.08759 j p1 = -0.01675 0.16555258711 j 18.5 3.7
-348.6678482663 p2 = -0.01675 -0.1655525871 j 19 3.8-7.288502767596 k1 = -0.16957525 19.5 3.9
A_q = -44.09656 20 4B_q = -44.60956 20.5 4.1K_q = -44.09656 21 4.2z1_q = -1.011634 21.5 4.316.264102069555 22 4.4
22.5 4.523 4.6
23.5 4.724 4.8
24.5 4.925 5
25.526
26.527
27.528
28.529
29.530
30.531
31.532
32.533
33.534
34.535
35.536
36.537
37.538
38.539
39.540
40.541
41.542
42.543
43.544
44.545
45.546
46.547
47.548
48.549
49.550
50.551
51.552
52.553
53.554
54.555
55.556
56.557
57.558
58.559
59.560
60.561
61.562
62.563
63.564
64.565
65.566
66.567
67.568
68.569
69.570
70.571
71.572
72.573
73.574
74.575
75.576
76.577
77.578
78.579
79.580
80.581
81.582
82.583
83.584
84.585
85.586
86.587
87.588
88.589
89.590
90.591
91.592
92.593
93.594
94.595
95.596
96.597
97.598
98.599
99.5100
100.5101
101.5102
102.5103
103.5104
104.5105
105.5106
106.5107
107.5108
108.5109
109.5110
110.5111
111.5112
112.5113
113.5114
114.5115
115.5116
116.5117
117.5118
118.5119
119.5120
120.5121
121.5122
122.5123
123.5124
124.5125
125.5126
126.5127
127.5128
128.5129
129.5130
130.5131
131.5132
132.5133
133.5134
134.5135
135.5136
136.5137
137.5138
138.5139
139.5140
140.5141
141.5142
142.5143
143.5144
144.5145
145.5146
146.5147
147.5148
148.5149
149.5150
150.5151
151.5152
152.5153
153.5154
154.5155
155.5156
156.5157
157.5158
158.5159
159.5160
160.5161
161.5162
162.5163
163.5164
164.5165
165.5166
166.5167
167.5168
168.5169
169.5170
170.5171
171.5172
172.5173
173.5174
174.5175
175.5176
176.5177
177.5178
178.5179
179.5180
180.5181
181.5182
182.5183
183.5184
184.5185
185.5186
186.5187
187.5188
188.5189
189.5190
190.5191
191.5192
192.5193
193.5194
194.5195
195.5196
196.5197
197.5198
198.5199
199.5200
Dutch Roll
Roll Delta_r Delta_ki
0 -0.0042 0.0016 -0.128454 -44.09656 0.1284540.441984 -73.8339 7.6068 -3.0854471 -19.40403 0.113042680.800681 -54.3634 3.5568 -3.5881876 0.001751 0.097111820.938815 -22.3248 -1.2489 -2.6422035 10.11787 0.080779360.982615 -3.403 -3.8162 -1.259459 11.98515 0.0641640.995287 2.8473 -4.5543 -0.1145647 8.923435 0.047384440.998762 2.9124 -4.4821 0.52086822 4.322938 0.030558510.999682 1.4617 -4.2521 0.67676836 0.469135 0.01380243
0.99992 0.378 -4.0999 0.53018776 -1.697895 -0.002770010.99998 -0.0722 -4.0431 0.27526754 -2.255971 -0.01904818
0.999995 -0.1438 -4.0377 0.04969406 -1.787367 -0.034925280.999999 -0.0886 -4.0474 -0.0846339 -0.941299 -0.05029905
1 -0.0307 -4.0558 -0.1261677 -0.183306 -0.065072371 -0.0014 -4.0597 -0.105342 0.27357 -0.079153891 0.0063 -4.0605 -0.0590184 0.419644 -0.092458461 0.005 -4.0602 -0.0149984 0.35451 -0.104907741 0.0022 -4.0598 0.01299997 0.201198 -0.11643052
delta_alphadelta_e
delta_qdelta_e
delta_thetadelta_e
0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.80
0.2
0.4
0.6
0.8
1
1.2
0 0.5 1 1.5 2 2.5 3 3.5
-80
-70
-60
-50
-40
-30
-20
-10
0
10
20
Delta_rDelta_ki
0.0004 -4.0595 0.02321936 0.053532 -0.12696313-0.0002 -4.0595 0.02072945 -0.041472 -0.13644976-0.0003 -4.0595 0.01245219 -0.077038 -0.14484271-0.0001 -4.0595 0.00394463 -0.069642 -0.15210256
0 -4.0595 -0.0018186 -0.042339 -0.158198330 -4.0595 -0.0042109 -0.013851 -0.163107540 -4.0595 -0.0040403 0.005664 -0.166816210 -4.0595 -0.0025911 0.013931 -0.169318850 -4.0595 -0.0009632 0.01355 -0.170618310 -4.0595 0.00020975 0.00879 -0.170725670 -4.0595 0.00075061 0.003349 -0.169659990 -4.0595 0.00077986 -0.000615 -0.167448070 -4.0595 0.00053254 -0.002475 -0.164124130 -4.0595 0.00022431 -0.002611 -0.159729430 -4.0595 -1.19E-05 -0.001803 -0.154311910 -4.0595 -0.000131 -0.000775 -0.147925730 -4.0595 -0.000149 2.23E-05 -0.140630790 -4.0595 -0.0001082 0.00043 -0.132492240 -4.0595 -5.052E-05 0.000498 -0.123579920 -4.0595 -3.43E-06 0.000366 -0.113967820 -4.0595 2.2276E-05 0.000174 -0.103733510 -4.0595 2.8178E-05 1.5E-05 -0.092957540 -4.0595 2.1767E-05 -7.27E-05 -0.081722830 -4.0595 1.1097E-05 -9.4E-05 -0.070114080 -4.0595 1.798E-06 -7.34E-05 -0.058217150 -4.0595 -3.655E-06 -3.8E-05 -0.046118440 -4.0595 -5.267E-06 -6.72E-06 -0.033904290 -4.0595 -4.334E-06 1.18E-05 -0.02166043
0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.80
0.2
0.4
0.6
0.8
1
1.2
0 1 2 3 4 5 6
-4
-3.5
-3
-2.5
-2
-1.5
-1
-0.5
0
0.5
1
D_alpha/D_e
0 1 2 3 4 5 6
-50
-40
-30
-20
-10
0
10
20
D_q/D_e
0 -4.0595 -2.389E-06 1.75E-05 -0.009471350 -4.0595 -5.702E-07 1.46E-05 0.002580240 -4.0595 5.6986E-07 8.15E-06 0.014413950 -4.0595 9.7232E-07 2.05E-06 0.025952210 -4.0595 8.5477E-07 -1.82E-06 0.037120770 -4.0595 5.0571E-07 -3.23E-06 0.04784914
0.058071050.067724780.076753520.085105740.092735350.099602030.105671330.110914870.115310380.118841810.121499260.12327903
0.12418350.124220980.123405630.121757210.119300850.116066850.112090290.107410790.10207213
0.0961219
0 1 2 3 4 5 6
-50
-40
-30
-20
-10
0
10
20
D_q/D_e
0 50 100 150 200 250
-0.2
-0.15
-0.1
-0.05
0
0.05
0.1
0.15
D_theta/D_e
0.089611060.082593590.075126070.067267180.059077350.050618260.04195241
0.03314270.02425195
0.01534250.00647578
-0.00228809-0.01089068-0.01927567-0.02738913-0.03517993-0.04259997
-0.0496045-0.05615238-0.06220626-0.06773282
-0.0727029-0.07709166-0.08087863-0.08404783-0.08658779-0.08849153-0.08975655
-0.09038479-0.09038251-0.08976021-0.08853245-0.08671771-0.08433819
-0.0814196-0.07799092-0.07408413-0.06973399
-0.0649777-0.05985463-0.05440604
-0.0486747-0.04270463-0.03654075-0.03022857-0.02381386-0.01734232-0.01085931-0.004409480.001963470.008217080.014310450.020204430.025861890.031247960.03633019
0.041078750.045466630.049469690.053066880.056240260.05897509
0.06125990.063086490.064449930.065348570.065783970.065760820.065286910.06437298
0.06303260.061282050.059140160.05662811
0.05376930.0505891
0.047114650.043374690.039399280.035219610.03086774
0.02637640.0217787
0.01710796
0.012397440.007680110.00298844
-0.00164579-0.00619176-0.01061973
-0.0149013-0.01900953-0.02291909-0.02660649
-0.0300501-0.03323035-0.03612981-0.03873323-0.04102769-0.04300256-0.04464961-0.04596299-0.04693923-0.04757722-0.04787822-0.04784575-0.04748558-0.04680562-0.04581585
-0.0445282-0.04295645-0.04111611
-0.03902427-0.03669944-0.03416146-0.03143128-0.02853081-0.02548278-0.02231057-0.01903798-0.01568914
-0.0122883-0.00885964-0.00542715-0.002014440.001355390.004659960.007877670.010987880.013971050.016808820.019484140.021981350.02428627
0.02638630.02827042
0.02992930.0313553
0.032542490.03348671
0.034185520.03463819
0.03484570.034810710.034537490.034031860.033301160.032354130.031200870.029852720.028322150.026622710.024768850.022775850.020659720.01843699
0.01612470.0137402
0.011301040.008824860.006329280.003831720.00134937
-0.00110102-0.00350314-0.00584133-0.00810061-0.01026679
-0.01232655-0.01426753-0.01607839-0.01774887-0.01926983-0.02063333-0.02183263-0.02286222-0.02371787-0.02439659-0.02489666-0.02521763-0.02536026-0.02532654-0.02511962-0.02474382
-0.0242045-0.02350808-0.02266196-0.02167442-0.02055459-0.01931234-0.01795824-0.01650343-0.01495956-0.01333871-0.01165327-0.00991588
-0.00813933-0.00633644-0.00452003-0.00270278-0.00089717
0.00088460.0026307
0.004329750.005970880.007543780.009038810.01044699
0.01176010.012970730.014072260.015058960.015925950.016669290.017285910.017773710.018131470.018358890.018456590.018426040.01826959
0.01799040.017592430.01708038
0.016459650.015736310.014917030.014009020.013019980.011958050.01083173
0.00964980.0084213
0.007155430.0058615
0.004548850.003226790.001904560.00059123
-0.00070434-0.00197357-0.00320817-0.00440025-0.00554235-0.00662745-0.00764906-0.00860122-0.00947856
-0.0102763-0.01099029-0.01161702-0.01215364
-0.01259797-0.0129485
-0.01320436-0.01336539-0.01343205-0.01340546-0.01328734-0.01308002-0.01278641-0.01240996-0.01195463-0.01142484-0.01082547
-0.0101618-0.00943943
-0.0086643-0.00784261-0.00698076-0.00608533-0.00516303-0.00422063-0.00326493-0.00230271-0.00134067-0.000385410.000556630.001479190.00237629
0.003242180.004071450.004859010.005600150.006290570.006926350.00750406
0.00802070.008473720.008861090.009181230.009433070.009616010.009729940.009775220.009752690.009663630.009509750.009293190.009016460.008682480.008294480.007856020.007370940.006843360.006277590.005678150.00504972
0.004397070.003725110.003038750.002342940.001642620.000942660.00024786-0.0004371
-0.00110768-0.00175953-0.00238847-0.00299059-0.00356218-0.00409984-0.00460045-0.00506118-0.00547953-0.00585334-0.00618079-0.00646039
0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.80
0.2
0.4
0.6
0.8
1
1.2
0 0.5 1 1.5 2 2.5 3 3.5
-80
-70
-60
-50
-40
-30
-20
-10
0
10
20
Delta_rDelta_ki
0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.80
0.2
0.4
0.6
0.8
1
1.2
0 1 2 3 4 5 6
-4
-3.5
-3
-2.5
-2
-1.5
-1
-0.5
0
0.5
1
D_alpha/D_e
0 1 2 3 4 5 6
-50
-40
-30
-20
-10
0
10
20
D_q/D_e
0 1 2 3 4 5 6
-50
-40
-30
-20
-10
0
10
20
D_q/D_e
0 50 100 150 200 250
-0.2
-0.15
-0.1
-0.05
0
0.05
0.1
0.15
D_theta/D_e
0.50290.047552 973.671 51388.19 68.8849810.575750.800686
4.584162.692853
1114.06 18.56767