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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Bibliographic Details
Main Author: Yeo, Andy Chia Guan
Other Authors: Ponnuthurai Nagaratnam Suganthan
Format: Final Year Project
Language:English
Published: 2017
Subjects:
Online Access:http://hdl.handle.net/10356/70869
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Institution: Nanyang Technological University
Language: English

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