Tractor 802

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