sc_attitude-master
所属分类：matlab编程
开发工具：matlab
文件大小：216KB
下载次数：2
上传日期：2017-08-01 18:07:13
上 传 者：
nab05
说明： Goal of this project is to simulate the rotational motion of a spacecraft in orbit. Plots of Euler angles and polhode curves (angular velocity time histories) are generated. Equations of Motion included in this package are for a rigid body in a torque-free environment and in circular orbit. See the EOM section under the Source Code Guide for more information.
The code is designed to be modular. Without getting very fancy, the user only needs to modify sc_attitude, sc_init, and sc_batch, depending on the experiment.
文件列表:
.DS_Store (12292, 2015-08-05)
LICENSE (1084, 2015-08-05)
ref (0, 2015-08-05)
ref\.DS_Store (6148, 2015-08-05)
ref\Reference Files (codes not for running) (0, 2015-08-05)
ref\Reference Files (codes not for running)\SC Linearized Equations (17045, 2015-08-05)
ref\Reference Files (codes not for running)\SC Linearized Equations C and q (15288, 2015-08-05)
ref\Reference Files (codes not for running)\SC Perturbed Equations (29997, 2015-08-05)
ref\Reference Files (codes not for running)\polhode_investigation_ICs (4915, 2015-08-05)
ref\Reference Files (codes not for running)\qcone.m (401, 2015-08-05)
ref\Reference Files (codes not for running)\rotationsequences_ref.m (2668, 2015-08-05)
ref\Reference Files (codes not for running)\savefiles.m (6330, 2015-08-05)
ref\Reference Files (codes not for running)\sc_equlibrium.m (3924, 2015-08-05)
ref\Reference Files (codes not for running)\sc_linearize.m (13026, 2015-08-05)
ref\Reference Files (codes not for running)\simple2DCM.m (1316, 2015-08-05)
v1 (0, 2015-08-05)
v1\.DS_Store (8196, 2015-08-05)
v1\EOM (0, 2015-08-05)
v1\EOM\sc_EOMC.m (1716, 2015-08-05)
v1\EOM\sc_gyrostat_EOMC.m (2911, 2015-08-05)
v1\EOM\sc_symmetricEOMq.m (1503, 2015-08-05)
v1\EOM\tf_EOMC.m (1282, 2015-08-05)
v1\EOM\tf_EOMq.m (947, 2015-08-05)
v1\Forces and Moments (0, 2015-08-05)
v1\Forces and Moments\eulerTF.m (577, 2015-08-05)
v1\Forces and Moments\f2_C.m (785, 2015-08-05)
v1\Forces and Moments\f2_q.m (1022, 2015-08-05)
v1\Forces and Moments\rotor.m (1168, 2015-08-05)
v1\General (0, 2015-08-05)
v1\General\DCM2q.m (582, 2015-08-05)
v1\General\DCM2simple.m (487, 2015-08-05)
v1\General\DCMrate.m (368, 2015-08-05)
v1\General\VERIFY_eom.m (2314, 2015-08-05)
v1\General\crossop.m (321, 2015-08-05)
v1\General\graph_titles.m (698, 2015-08-05)
v1\General\q2DCM.m (749, 2015-08-05)
v1\General\q2simple.m (321, 2015-08-05)
... ...
sc_attitude
===========
Spacecraft Attitude Simulation
v1: first working version
v2: updated to comply with personal code style standard
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