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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2017
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Article
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Tab 1
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Research Article
A Shape-Based Method for Continuous Low-Thrust Trajectory Design between Circular Coplanar Orbits
Table 1
Boundary conditions and input parameters for Earth-Mars rendezvous orbit.
Boundary conditions
Input parameters
1 DU
1
0 rad
6
1.5234 DU
6
3.548 rad
13.45 TU
0 DU/TU
151
1 rad/TU
0 DU/TU
0.5318 rad/TU