277a7258-65a5-482f-ab5f-cc4d492c78ee
101 |maca64
102 |%<Auto>
104 |%<Auto>
105 |%<AutoIncrement:4.0>
106 |normal
109 | 119 |warning
122 |5
873 |off
876 |off
877 |-1
878 |inherit
879 |off
883 |off
884 |-1
885 |inherit
886 |off
890 |off
891 |-1
892 |inherit
893 |off
897 |off
898 |-1
899 |inherit
900 |off
904 |off
905 |-1
906 |inherit
907 |11
909 |off
912 |Xe
913 |inherit
914 |off
915 |off
919 |Ve
920 |inherit
921 |off
922 |off
926 |Vt
927 |inherit
928 |off
929 |off
933 |alpha
934 |inherit
935 |off
936 |off
940 |beta
941 |inherit
942 |off
943 |off
947 |EA
948 |inherit
949 |off
950 |off
954 |gamma
955 |inherit
956 |off
957 |off
961 |om
962 |inherit
963 |off
964 |off
968 |accl
969 |inherit
970 |off
971 |off
975 |ang accl
976 |inherit
977 |off
978 |off
982 |inherit
983 |off
984 |0
987 |0
988 |0
989 |0
990 |0
991 |0
992 |0
993 |Unset
994 |0
995 |VariableStepAuto
996 |0
997 |Simulink
998 |0
999 |5
1000 |shared6dof/6DOF (Euler Angles)
1002 |$bdroot/Nonlinear F16 Model/6DOF (Quaternion)
1003 |192
1004 |LIBRARY_BLOCK
1005 |aerolibasang/Dynamic Pressure
1008 |$bdroot/Nonlinear F16 Model/Dynamic Pressure
1009 |26
1010 |LIBRARY_BLOCK
1011 |aerolibatmos2/ISA Atmosphere Model
1014 |$bdroot/Nonlinear F16 Model/ISA Atmosphere Model
1015 |5
1016 |LIBRARY_BLOCK
1017 |aerolibasang/Incidence, Sideslip, 1020 | & Airspeed
1021 |$bdroot/Nonlinear F16 Model/Incidence, Sideslip, & Airspeed
1022 |7
1023 |LIBRARY_BLOCK
1024 |aerolibasang/Mach Number
1027 |$bdroot/Nonlinear F16 Model/Mach Number
1028 |200
1029 |LIBRARY_BLOCK
1030 |1
1032 |ode23t
1046 |Nonlinear F16 Model/Transform weight vector to body axis
1409 |[422 539.941 189 413]
1410 |[0 156.75 0 153.75]
1411 |[1 1 3600 1200 1.180555555555556]
1412 |8
1413 |6
1414 |CLUSTER_CHART
1415 |EML_CHART
1416 |1
1417 |1
1418 |fcn
1420 |eML_blk_kernel()
1424 |[18 64.5 118 66]
1425 |12
1426 |SUBCHART
1427 |8
1428 |FUNC_STATE
1429 |CLUSTER_STATE
1430 |1
1432 |function Wb = fcn(We,DCM_be) 1433 | Wb = DCM_be*We; % Weight in body coordinate system. DCM_be is correct, no need for transpose. They must have fixed it in this version. 1434 |
1435 |1
1436 |INPUT_DATA
1440 |-1
1443 |SF_INHERITED_TYPE
1446 |SF_DOUBLE_TYPE
1447 |SF_COMPLEX_INHERITED
1449 |inherit
1451 |Inherit: Same as Simulink
1454 | 1455 | 1456 |OUTPUT_DATA
1457 |-1
1460 |SF_INHERITED_TYPE
1463 |SF_DOUBLE_TYPE
1464 |SF_COMPLEX_INHERITED
1466 |SF_FRAME_NO
1467 |inherit
1469 |Inherit: Same as Simulink
1472 | 1473 | 1474 |INPUT_DATA
1475 |-1
1478 |SF_INHERITED_TYPE
1481 |SF_DOUBLE_TYPE
1482 |1
1483 |16
1484 |SF_COMPLEX_INHERITED
1486 |SF_FRAME_INHERITED
1487 |inherit
1489 |Inherit: Same as Simulink
1492 | 1493 |{eML_blk_kernel();}
1495 |[28.125 13.875 102.544 14.964]
1496 |12
1497 |[0 0 1 0 23.5747 14.625 0 0]
1499 |3
1502 |[1 0 -1 0 23.5747 42.5747 0 0]
1503 |[23.5747 24.9468]
1505 |[21.175 25.975 14.625 42.575]
1506 |8
1507 |SMART
1508 |BOTH_STICK
1510 |1
1512 |[23.5747 49.5747 7]
1515 |8
1516 |CONNECTIVE_JUNCTION
1517 |80000049
1526 |Default Simulink S-Function Target.
1529 |7
1535 |Nonlinear F16 Model/Transform weight vector to body axis
1536 |8
1537 |[223, 338, 826, 833]
1557 |40
1558 |[20, 101, 40, 119]
1560 |-1
1561 |[20, 136, 40, 154]
1564 |13
1565 |2
1566 |[1, 1]
1569 |[270, 230, 320, 270]
1570 |30
1571 |1
1572 |Stateflow S-Function 1
1575 |[2, 2]
1576 |[180, 100, 230, 160]
1577 |29
1578 |sf_sfun
1579 |[2 2]
1580 |off
1581 |on
1582 |off
1583 |2
1585 |Wb
1586 |[460, 241, 480, 259]
1590 |31
1591 |[460, 101, 480, 119]
1594 |-5
1595 |39
1598 |122::1#out:1
1599 |[120, 0]
1600 |122::38#in:1
1601 |40
1604 |122::22#out:1
1605 |122::38#in:2
1606 |Wb
1609 |41
1610 |[0, 0]
1611 |122::38#out:2
1612 |122::5#in:1
1613 |42
1616 |122::39#out:1
1617 |122::40#in:1
1618 |43
1621 |122::38#out:1
1622 |122::39#in:1
1623 |[887, 25, 2144, 1030]
1630 |189
1631 |[-235, -222, -205, -208]
1633 |-1
1634 |[-235, -192, -205, -178]
1637 |1
1638 |2
1639 |[-235, -162, -205, -148]
1642 |2
1643 |3
1644 |[-235, -132, -205, -118]
1647 |3
1648 |4
1649 |[-235, -102, -205, -88]
1652 |4
1653 |5
1654 |[-235, -72, -205, -58]
1657 |5
1658 |6
1659 |[-235, -42, -205, -28]
1662 |6
1663 |7
1664 |[-235, -12, -205, 2]
1667 |8
1668 |8
1669 |[-235, 18, -205, 32]
1672 |9
1673 |9
1674 |[1, 2]
1677 |[260, -94, 265, -56]
1678 |12
1679 |2
1680 |[1, 1]
1683 |[75, -95, 145, -65]
1684 |11
1685 |F16AeroFM
1686 |6
1687 |[9, 1]
1690 |[-85, -277, -75, 117]
1691 |10
1692 |9
1693 |bar
1694 |[350, -172, 380, -158]
1697 |-2
1698 |3
1699 |[350, -12, 380, 2]
1702 |7
1703 |2
1704 |3
1705 |2
1708 |264#out:1
1709 |271#in:4
1710 |3
1713 |263#out:1
1714 |[59, 0; 0, -15]
1715 |271#in:3
1716 |4
1719 |265#out:1
1720 |[71, 0; 0, 15]
1721 |271#in:5
1722 |5
1725 |262#out:1
1726 |[49, 0; 0, -30]
1727 |271#in:2
1728 |6
1731 |266#out:1
1732 |[60, 0; 0, 30]
1733 |271#in:6
1734 |7
1737 |260#out:1
1738 |[40, 0; 0, -45]
1739 |271#in:1
1740 |8
1743 |267#out:1
1744 |[49, 0; 0, 45]
1745 |271#in:7
1746 |9
1749 |269#out:1
1750 |[39, 0; 0, 60]
1751 |271#in:8
1752 |10
1755 |270#out:1
1756 |[28, 0; 0, 75]
1757 |271#in:9
1758 |12
1761 |271#out:1
1762 |272#in:1
1763 |13
1766 |273#out:1
1767 |[38, 0; 0, -80]
1768 |261#in:1
1769 |14
1772 |273#out:2
1773 |[38, 0; 0, 60]
1774 |268#in:1
1775 |15
1778 |272#out:1
1779 |[48, 0; 0, 5]
1780 |273#in:1
1781 |[1972, 87, 3456, 1090]
1788 |73
1789 |[715, 618, 745, 632]
1791 |165
1792 |3
1793 |[105, 68, 135, 82]
1796 |168
1797 |2
1798 |3
1799 |[105, 243, 135, 257]
1802 |167
1803 |3
1804 |3
1805 |[780, 163, 810, 177]
1808 |182
1809 |4
1810 |[780, 198, 810, 212]
1813 |183
1814 |5
1815 |[780, 233, 810, 247]
1818 |184
1819 |6
1820 |[780, 268, 810, 282]
1823 |197
1824 |7
1825 |[2, 8]
1828 |[295, 6, 490, 279]
1829 |169
1830 |6.0
1831 |shared6dof/6DOF (Euler Angles)
1832 |6DOF EoM (Body Axis)
1833 |Inherit from model
1835 |Inherit from model
1836 |Inherit from model
1837 |Inherit from model
1838 |Inherit from model
1839 |on
1840 |Metric (MKS)
1841 |Fixed
1842 |Euler Angles
1843 |IC.inertial_position
1844 |IC.body_velocity
1845 |IC.euler_angles
1846 |IC.omega
1847 |Param.mass
1848 |0.5
1849 |2.0
1850 |Param.moi
1851 |eye(3)
1852 |2*eye(3)
1853 |1.0
1854 |on
1855 |off
1856 |0
1857 |{'Xe', 'Ye', 'Ze'}
1858 |{'U', 'v', 'w'}
1859 |''
1860 |{'qr', 'qi', 'qj', 'qk'}
1861 |{'p', 'q', 'r'}
1862 |''
1863 |[1235, 475, 1265, 505]
1867 |204
1868 |off
1869 |[2, 1]
1872 |[1290, 212, 1315, 288]
1873 |98
1874 |rectangular
1875 |+-
1876 |[3, 1]
1879 |[230, 28, 265, 122]
1880 |144
1881 |rectangular
1882 |+++
1883 |[105, 495, 160, 525]
1886 |130
1887 |Param.g
1888 |[105, 445, 135, 475]
1891 |143
1892 |0
1893 |[2, 1]
1896 |[820, 391, 880, 464]
1897 |54
1898 |6.0
1899 |aerolibasang/Dynamic Pressure
1900 |Dynamic Pressure
1901 |Inherit from model
1903 |Inherit from model
1904 |Inherit from model
1905 |Inherit from model
1906 |Inherit from model
1907 |on
1908 |[9, 2]
1912 |[895, -27, 955, 297]
1913 |203
1914 |on
1915 |[765, 20, 825, 40]
1919 |116
1920 |alpha
1921 |[765, -15, 825, 5]
1924 |161
1925 |Vt
1926 |[1135, 85, 1195, 105]
1929 |85
1930 |alpha
1931 |[1135, 220, 1195, 240]
1934 |156
1935 |euler_ang
1936 |[1135, 120, 1195, 140]
1939 |87
1940 |beta
1941 |[1135, 260, 1195, 280]
1944 |97
1945 |alpha
1946 |[705, 580, 765, 600]
1949 |94
1950 |Vb
1951 |[1455, -20, 1515, 0]
1954 |101
1955 |omega
1956 |[1455, 15, 1515, 35]
1959 |103
1960 |lin_accl
1961 |[155, 35, 210, 55]
1964 |123
1965 |Faero
1966 |[155, 200, 210, 220]
1969 |124
1970 |Maero
1971 |[345, 520, 415, 540]
1974 |142
1975 |DCM_be
1976 |[730, 398, 775, 422]
1979 |57
1980 |Vb
1981 |[1455, 110, 1515, 130]
1984 |179
1985 |off
1986 |off
1987 |Vb
1988 |[155, 95, 210, 115]
1991 |146
1992 |Weight
1993 |1
1995 |Wb
1996 |[765, 55, 825, 75]
2000 |157
2001 |beta
2002 |[765, 90, 825, 110]
2005 |158
2006 |omega
2007 |[1455, 135, 1515, 155]
2010 |180
2011 |a
2012 |[730, 435, 775, 455]
2015 |58
2016 |rho
2017 |[1135, 15, 1195, 35]
2020 |172
2021 |Ve
2022 |[1455, 50, 1520, 70]
2025 |174
2026 |off
2027 |off
2028 |ang_accl
2029 |[1035, 475, 1075, 505]
2032 |73
2033 |Xe
2034 |[765, 125, 825, 145]
2037 |118
2038 |qbar
2039 |[1135, -20, 1195, 0]
2042 |81
2043 |Xe
2044 |[1135, 50, 1195, 70]
2047 |83
2048 |Vt
2049 |[945, 542, 985, 568]
2052 |38
2053 |alpha
2054 |[550, 217, 620, 243]
2057 |170
2058 |off
2059 |off
2060 |ang_accl
2061 |[550, 182, 620, 208]
2064 |67
2065 |off
2066 |off
2067 |omega
2068 |[550, 252, 620, 278]
2071 |69
2072 |off
2073 |off
2074 |lin_accl
2075 |[550, 42, 620, 68]
2078 |71
2079 |off
2080 |off
2081 |Xe
2082 |[550, 77, 620, 103]
2085 |72
2086 |off
2087 |off
2088 |euler_ang
2089 |[550, 147, 620, 173]
2092 |93
2093 |off
2094 |off
2095 |Vb
2096 |[980, 42, 1050, 68]
2099 |125
2100 |off
2101 |off
2102 |Faero
2103 |[980, 202, 1050, 228]
2106 |127
2107 |Maero
2108 |[550, 7, 620, 33]
2111 |171
2112 |off
2113 |off
2114 |Ve
2115 |[580, 497, 650, 523]
2118 |138
2119 |Weight
2120 |[1540, 550, 1625, 580]
2123 |44
2124 |rho
2125 |[1540, 450, 1625, 480]
2128 |178
2129 |a
2130 |[945, 577, 985, 603]
2133 |55
2134 |beta
2135 |[945, 612, 985, 638]
2138 |56
2139 |Vt
2140 |[915, 417, 955, 443]
2143 |59
2144 |qbar
2145 |[550, 112, 620, 138]
2148 |66
2149 |off
2150 |off
2151 |DCM_be
2152 |[1, 4]
2155 |[1360, 387, 1505, 593]
2156 |33
2157 |off
2158 |6.0
2159 |aerolibatmos2/ISA Atmosphere Model
2160 |International Standard Atmosphere Model
2161 |Inherit from model
2163 |Inherit from model
2164 |Inherit from model
2165 |Inherit from model
2166 |Inherit from model
2167 |on
2168 |off
2169 |9.80665
2170 |1.4
2171 |287.0531
2172 |0.0065
2173 |11000
2174 |20000
2175 |1.225
2176 |101325
2177 |288.15
2178 |0
2179 |[1, 3]
2183 |[825, 540, 885, 640]
2184 |35
2185 |6.0
2186 |aerolibasang/Incidence, Sideslip, 2187 | & Airspeed
2188 |Incidence,Sideslip,&Airspeed
2189 |Inherit from model
2191 |Inherit from model
2192 |Inherit from model
2193 |Inherit from model
2194 |Inherit from model
2195 |on
2196 |[2, 1]
2200 |[1540, 107, 1600, 158]
2201 |177
2202 |off
2203 |off
2204 |6.0
2205 |aerolibasang/Mach Number
2206 |Mach Number
2207 |Inherit from model
2209 |Inherit from model
2210 |Inherit from model
2211 |Inherit from model
2212 |Inherit from model
2213 |on
2214 |[3, 1]
2218 |[310, 448, 315, 522]
2219 |133
2220 |3
2221 |bar
2222 |[1, 1]
2225 |[1100, 471, 1140, 509]
2226 |39
2227 |3
2228 |Index vector (dialog)
2229 |3
2230 |1
2231 |[1, 1]
2234 |[1220, 211, 1260, 249]
2235 |95
2236 |3
2237 |Index vector (dialog)
2238 |2
2239 |1
2240 |[2, 1]
2243 |[780, 580, 800, 600]
2244 |164
2245 ||++
2246 |[2, 1]
2249 |[235, 200, 255, 220]
2250 |166
2251 |off
2252 |off
2253 ||++
2254 |[1540, 405, 1560, 425]
2257 |147
2258 |[1540, 505, 1560, 525]
2261 |148
2262 |[2, 1]
2265 |[450, 464, 545, 551]
2266 |141
2267 |Stateflow.Translate.translate
2268 |ExplicitOnly
2269 |on
2270 |MATLAB Function
2271 |on
2272 |1
2274 |Wb
2275 |[185, 485, 265, 535]
2280 |132
2281 |Param.mass
2282 |[1230, -17, 1260, -3]
2285 |108
2286 |[1230, 18, 1260, 32]
2289 |173
2290 |2
2291 |[1230, 53, 1260, 67]
2294 |109
2295 |3
2296 |[1230, 88, 1260, 102]
2299 |110
2300 |4
2301 |[1230, 123, 1260, 137]
2304 |111
2305 |5
2306 |[1360, 183, 1390, 197]
2309 |160
2310 |6
2311 |[1360, 243, 1390, 257]
2314 |112
2315 |7
2316 |[1550, -17, 1580, -3]
2319 |113
2320 |8
2321 |[1550, 18, 1580, 32]
2324 |114
2325 |9
2326 |[1555, 53, 1585, 67]
2329 |175
2330 |10
2331 |[1625, 128, 1655, 142]
2334 |181
2335 |11
2336 |60
2339 |50#out:1
2340 |11#in:1
2341 |96
2344 |65#out:1
2345 |[30, 0]
2346 |92#in:1
2347 |37
2350 |7#out:3
2351 |28#in:1
2352 |156
2355 |5#out:3
2356 |131#in:1
2357 |155
2360 |5#out:1
2361 |130#in:1
2362 |25
2365 |5#out:4
2366 |16#in:1
2367 |40
2370 |30#out:1
2371 |26#in:2
2372 |99
2375 |81#out:1
2376 |[30, 0]
2377 |95#in:1
2378 |95
2381 |62#out:1
2382 |[30, 0]
2383 |91#in:1
2384 |310
2387 |5#out:2
2388 |201#in:1
2389 |39
2392 |29#out:1
2393 |26#in:1
2394 |97
2397 |77#out:1
2398 |93#in:1
2399 |94
2402 |60#out:1
2403 |90#in:1
2404 |38
2407 |7#out:2
2408 |27#in:1
2409 |84
2412 |75#out:1
2413 |77#in:1
2414 |12
2417 |7#out:1
2418 |10#in:1
2419 |13
2422 |11#out:1
2423 |274#in:1
2424 |83
2427 |76#out:1
2428 |77#in:2
2429 |183
2432 |157#out:1
2433 |[4, 0]
2434 |187
2436 |[0, -40]
2437 |174#in:1
2438 |186
2441 |75#in:1
2442 |98
2446 |79#out:1
2447 |[30, 0]
2448 |94#in:1
2449 |42
2452 |26#out:1
2453 |31#in:1
2454 |93
2457 |59#out:1
2458 |[30, 0]
2459 |89#in:1
2460 |123
2463 |111#out:1
2464 |113#in:1
2465 |462
2468 |113#out:1
2469 |114#in:3
2470 |145
2473 |114#out:1
2474 |122#in:1
2475 |146
2478 |122#out:1
2479 |119#in:1
2480 |147
2483 |123#out:1
2484 |122#in:2
2485 |148
2488 |124#out:1
2489 |[119, 0]
2490 |150
2492 |[0, 25]
2493 |114#in:2
2494 |149
2497 |114#in:1
2498 |151
2502 |103#out:1
2503 |126#in:1
2504 |276
2507 |187#out:1
2508 |126#in:2
2509 |153
2512 |128#out:1
2513 |126#in:3
2514 |293
2517 |126#out:1
2518 |192#in:1
2519 |268
2522 |72#out:1
2523 |182#in:1
2524 |269
2527 |182#out:1
2528 |7#in:1
2529 |270
2532 |183#out:1
2533 |[40, 0]
2534 |182#in:2
2535 |272
2538 |104#out:1
2539 |185#in:1
2540 |275
2543 |186#out:1
2544 |[105, 0]
2545 |185#in:2
2546 |305
2549 |192#out:1
2550 |194#in:1
2551 |297
2554 |192#out:2
2555 |[55, 0]
2556 |48#in:1
2557 |298
2560 |192#out:3
2561 |[55, 0]
2562 |49#in:1
2563 |299
2566 |192#out:4
2567 |[55, 0]
2568 |43#in:1
2569 |300
2572 |192#out:5
2573 |[55, 0]
2574 |71#in:1
2575 |301
2578 |192#out:6
2579 |[55, 0]
2580 |44#in:1
2581 |304
2584 |192#out:7
2585 |193#in:1
2586 |303
2589 |192#out:8
2590 |[55, 0]
2591 |46#in:1
2592 |306
2595 |195#out:1
2596 |196#in:1
2597 |307
2600 |197#out:1
2601 |198#in:1
2602 |311
2605 |202#out:1
2606 |200#in:1
2607 |312
2610 |203#out:1
2611 |200#in:2
2612 |313
2615 |200#out:1
2616 |204#in:1
2617 |578
2620 |259#out:1
2621 |105#in:1
2622 |461
2625 |185#out:1
2626 |192#in:2
2627 |579
2630 |259#out:2
2631 |107#in:1
2632 |569
2635 |179#out:1
2636 |259#in:1
2637 |570
2640 |9#out:1
2641 |259#in:2
2642 |571
2645 |169#out:1
2646 |259#in:3
2647 |572
2650 |170#out:1
2651 |259#in:4
2652 |573
2655 |51#out:1
2656 |259#in:5
2657 |574
2660 |212#out:1
2661 |259#in:6
2662 |575
2665 |213#out:1
2666 |259#in:7
2667 |576
2670 |214#out:1
2671 |259#in:8
2672 |577
2675 |242#out:1
2676 |259#in:9
2677 |590
2680 |274#out:1
2681 |5#in:1
2682 |Gravity
2685 |[87, 354, 669, 652]
2686 |[0, 0, 0, 0]
2687 |on
2688 |on
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2696 |<!DOCTYPE HTML PUBLIC "-//W3C//DTD HTML 4.0//EN" "http://www.w3.org/TR/REC-html40/strict.dtd"> 2699 | <html><head><meta name="qrichtext" content="1" /><style type="text/css"> 2700 | p, li { white-space: pre-wrap; } 2701 | </style></head><body align="left" style=" font-family:'Helvetica'; font-size:10px; font-weight:400; font-style:normal;"> 2702 | <p align="left" style=" margin-top:0px; margin-bottom:0px; margin-left:0px; margin-right:0px; -qt-block-indent:0; text-indent:0px;"><span style=" font-size:18px; font-weight:600;">Nonlinear Model of the F16 Aircraft</span></p> 2703 | <p align="left" style="-qt-paragraph-type:empty; margin-top:0px; margin-bottom:0px; margin-left:0px; margin-right:0px; -qt-block-indent:0; text-indent:0px; font-size:12px;"><br /></p> 2704 | <p align="left" style=" margin-top:0px; margin-bottom:0px; margin-left:0px; margin-right:0px; -qt-block-indent:0; text-indent:0px;"><span style=" font-size:12px;">Developed by Raktim Bhattacharya</span></p> 2705 | <p align="left" style=" margin-top:0px; margin-bottom:0px; margin-left:0px; margin-right:0px; -qt-block-indent:0; text-indent:0px;"><span style=" font-size:12px;">Professor, Aerospace Engineering,</span></p> 2706 | <p align="left" style=" margin-top:0px; margin-bottom:0px; margin-left:0px; margin-right:0px; -qt-block-indent:0; text-indent:0px;"><span style=" font-size:12px;">Texas A&M University.</span></p></body></html>
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3082 |<!DOCTYPE HTML PUBLIC "-//W3C//DTD HTML 4.0//EN" "http://www.w3.org/TR/REC-html40/strict.dtd"> 3085 | <html><head><meta name="qrichtext" content="1" /><style type="text/css"> 3086 | p, li { white-space: pre-wrap; } 3087 | </style></head><body align="left" style=" font-family:'Helvetica'; font-size:10px; font-weight:400; font-style:normal;"> 3088 | <p align="left" style=" margin-top:0px; margin-bottom:0px; margin-left:0px; margin-right:0px; -qt-block-indent:0; text-indent:0px;"><span style=" font-size:18px; font-weight:600;">Nonlinear Model of the F16 Aircraft</span></p> 3089 | <p align="left" style="-qt-paragraph-type:empty; margin-top:0px; margin-bottom:0px; margin-left:0px; margin-right:0px; -qt-block-indent:0; text-indent:0px; font-size:12px;"><br /></p> 3090 | <p align="center" style=" margin-top:0px; margin-bottom:0px; margin-left:0px; margin-right:0px; -qt-block-indent:0; text-indent:0px;"><span style=" font-size:10px;">Developed by </span></p> 3091 | <p align="center" style="-qt-paragraph-type:empty; margin-top:0px; margin-bottom:0px; margin-left:0px; margin-right:0px; -qt-block-indent:0; text-indent:0px;"><br /></p> 3092 | <p align="center" style=" margin-top:0px; margin-bottom:0px; margin-left:0px; margin-right:0px; -qt-block-indent:0; text-indent:0px;"><span style=" font-size:10px;">Raktim Bhattacharya</span></p> 3093 | <p align="center" style=" margin-top:0px; margin-bottom:0px; margin-left:0px; margin-right:0px; -qt-block-indent:0; text-indent:0px;"><span style=" font-size:10px; font-style:italic;">Professor, </span></p> 3094 | <p align="center" style=" margin-top:0px; margin-bottom:0px; margin-left:0px; margin-right:0px; -qt-block-indent:0; text-indent:0px;"><span style=" font-size:10px;">Aerospace Engineering,Texas A&M University.</span></p></body></html>
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