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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2019
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Article
/
Tab 2
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Research Article
Low-Thrust Trajectory Design Using Finite Fourier Series Approximation of Pseudoequinoctial Elements
Table 2
Settings of the number of terms for the Earth-Mars rendezvous trajectory.
No.
1
2
3
4
5
6
7
8
4
4
3
4
3
3
3
3
3
3
3
2
4
4
3
2
2
2
3
2
2
2
2
2
5
4
4
5
5
4
5
6
