http://www.cnr.it/ontology/cnr/individuo/prodotto/ID303219
MOID-increasing disposal strategies for LPO missions (Contributo in atti di convegno)
- Type
- Label
- MOID-increasing disposal strategies for LPO missions (Contributo in atti di convegno) (literal)
- Anno
- 2014-01-01T00:00:00+01:00 (literal)
- Alternative label
E.M. Alessi, J.P. Sánchez Cuartielles (2014)
MOID-increasing disposal strategies for LPO missions
in 65th International Astronautical Congress, Toronto, Canada, 29/9/2014-3/10/2014
(literal)
- Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#autori
- E.M. Alessi, J.P. Sánchez Cuartielles (literal)
- Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#affiliazioni
- IFAC-CNR (Italy), Universitat Politècnica de Catalunya (Spain) (literal)
- Titolo
- MOID-increasing disposal strategies for LPO missions (literal)
- Abstract
- The issue on the final fate of Sun--Earth Libration Point Orbits (LPO) missions, commonly chosen to place space observatories, has
recently drawn the attention of ESA. So far, the only disposal concept implemented at the end-of-life
consists in moving the spacecraft on a heliocentric graveyard orbit.
This idea requires that the spacecraft will never return to Earth after leaving
its operational orbit. A na\"ive approach to fulfill this constraint is to close the zero velocity curves, in
such a way that no physical motion is possible between the geocentric orbital regime and the heliocentric
one. We propose here an alternative strategy: the disposal
orbit is such that, despite the fact that the given bottleneck passage may remain open, it always has an
increasing Minimum Orbit Intersection Distance (MOID) evolution.
Two numerical procedures have been developed to this end: one considers the application of optimization
techniques, the other uses the Newton's method. Both methodologies aim to design spacecraft--Earth encounters,
which ensure that the variation of the average orbital elements are such that the
MOID will increase. The evolution of the orbital elements as a function of the angle of encounter is first analyzed
by means of a semi-analytical 3D extension of the Keplerian map \cite{RS}, which provides a first guess solution to the numerical procedures. (literal)
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