Spacecraft trajectory optimization using evolutionary algorithm
Spacecraft and space systems are complex and generally difficult to design. The computation for the trajectory is no exception. For such nonlinear optimal control problems, they generally do not have any analytical solutions and hence the model for the computation are very difficult to design. Evolu...
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| Format: | Final Year Project (FYP) |
| Language: | English |
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2017
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| Online Access: | http://hdl.handle.net/10356/70869 |