Abstract
An approach to basic trajectory design, which allows extension of the classical two-impulse transfer strategy by using the planetary swingby techniques was studied. This approach can effectively reduce the launch energy and the total velocity increments, thereby including a large number of potentially accessible targets. This work presents a significant reference for mission designer when selecting the scientifically significant and technically feasible target for a space mission.
| Original language | English |
|---|---|
| Pages (from-to) | 502-505 |
| Number of pages | 4 |
| Journal | Journal of Guidance, Control, and Dynamics |
| Volume | 29 |
| Issue number | 2 |
| DOIs | |
| State | Published - 2006 |
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