aircraft-6-DOF-simulation
所属分类：matlab编程
开发工具：matlab
文件大小：91KB
下载次数：346
上传日期：2013-04-02 21:03:23
上 传 者：
lvzheng0407
说明： 飞行器六自由度建模，以及飞行器配平，线性化的matlab程序
(The aircraft six degrees of freedom modeling, as well as aircraft trim, linearization matlab program)
文件列表:
HW4-7.m (68, 2011-12-15)
HW4_7.m (74, 2011-12-15)
HW4_71.m (179, 2011-12-16)
Untitled.m (437, 2011-12-13)
Untitled2.m (96, 2011-12-13)
fem2.m (9769, 2012-02-16)
main.m (1071, 2012-01-09)
myfun.m (118, 2011-12-16)
step1.jpg (25932, 2012-01-09)
step1.m (271, 2012-01-06)
step2.jpg (25677, 2012-01-09)
step2.m (248, 2012-01-06)
totle.jpg (68169, 2012-01-09)
totle.m (876, 2012-01-09)
zn.m (873, 2012-01-07)
发动机推力指数 (0, 2013-03-28)
发动机推力指数\theottleidle.m (90, 2011-12-27)
发动机推力指数\throttledelt.m (81, 2011-12-20)
发动机推力指数\throttlemaximum.m (98, 2011-12-27)
发动机推力指数\throttlemilitary.m (93, 2011-12-27)
标准大气模型 (0, 2013-03-28)
标准大气模型\ADC.m (247, 2013-03-28)
算气动指数alpha=1.038，beta=0 (0, 2013-04-01)
算气动指数alpha=1.038，beta=0\A.m (159, 2012-01-06)
算气动指数alpha=1.038，beta=0\Clda.m (725, 2012-01-06)
算气动指数alpha=1.038，beta=0\Cldr.m (626, 2012-01-06)
算气动指数alpha=1.038，beta=0\Clp.m (161, 2012-01-06)
算气动指数alpha=1.038，beta=0\Clr.m (154, 2012-01-06)
算气动指数alpha=1.038，beta=0\Cm.m (531, 2012-01-06)
算气动指数alpha=1.038，beta=0\Cmq.m (151, 2012-01-06)
算气动指数alpha=1.038，beta=0\Cnda.m (743, 2012-01-06)
算气动指数alpha=1.038，beta=0\Cndr.m (721, 2012-01-06)
算气动指数alpha=1.038，beta=0\Cnp.m (154, 2012-01-06)
算气动指数alpha=1.038，beta=0\Cnr.m (164, 2012-01-06)
算气动指数alpha=1.038，beta=0\Cx.m (525, 2012-01-06)
算气动指数alpha=1.038，beta=0\Cxde.m (107, 2011-12-20)
算气动指数alpha=1.038，beta=0\Cyp.m (159, 2012-01-06)
算气动指数alpha=1.038，beta=0\Cyr.m (155, 2012-01-06)
算气动指数alpha=1.038，beta=0\Czq.m (157, 2012-01-06)
算气动指数alpha=1.038，beta=0\interp111.m (560, 2011-12-20)
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