| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 10680847 | Acta Astronautica | 2014 | 12 Pages |
Abstract
⺠The paper describes the fuel-optimal low-thrust transfer problem with bounded control. ⺠A reference solution for a transfer to the asteroid 1996FG3 is identified. ⺠An algorithm for expanding the solution in the boundary conditions is presented. ⺠The algorithm is applied to the high order optimal feedback of the transfer to 1996FG3. ⺠The algorithm is able to manage a maximum initial and final position error of 10â3 AU.
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Authors
P. Di Lizia, R. Armellin, A. Morselli, F. Bernelli-Zazzera,