航天器最优控制理论,是在满足一定约束条件下,寻求最优控制策略,使得性能指标取极大值或极小值。以航天器交会对接最优制导律设计与仿真为例,阐释最优控制的算法流程以及设计思想...">
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Spacecraft optimal control theory, as well as optimal guidance law

iprize
2014-09-01 23:07:47
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space:nowrap;">航天器最优控制理论,是在满足一定约束条件下,寻求最优控制策略,使得性能指标取极大值或极小值。航天器交会对接最优制导律设计与仿真为例,阐释最优控制的算法流程以及设计思想
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Name Size Date
fuyuan.asv74.00 B06-12-13|09:31
fuyuan.m155.00 B06-12-13|11:41
lazhi.asv107.00 B06-12-13|09:21
lazhi.m147.00 B06-12-13|11:41
riccatiequation.asv46.00 B06-12-13|09:01
riccatiequation.m131.00 B06-12-13|09:04
simulation.asv3.77 kB06-12-13|11:37
simulation.m3.79 kB06-12-13|11:42
stateequation.asv109.00 B05-12-13|20:54
stateequation.m111.00 B06-12-13|08:23
simulation02.m3.98 kB08-12-13|11:36
stateequation.m127.00 B08-12-13|09:06
算例030.00 B09-12-13|15:16
算例040.00 B09-12-13|15:16
航天器交会对接最优制导律设计与仿真0.00 B09-12-13|15:17
...
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Spacecraft optimal control theory, as well as optimal guidance law (7.57 kB)

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