| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 1716723 | Acta Astronautica | 2007 | 5 Pages |
Abstract
The paper presents the solution of the first ACT global trajectory optimisation competition problem on the transfer of a spacecraft from Earth to asteroid 2001 TW-229. The initial optimal control problem is reduced to an auxiliary mathematical programming problem by means of simplifying assumptions. The auxiliary problem is solved numerically with the use of a decomposition method. The solution is then employed to construct the Pontrjagin extremals of the initial problem.
Keywords
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
I.S. Grigoriev, M.P. Zapletin, E.V. Zapletina,