An impulsive model predictive static programming based station-keeping guidance for quasi-halo orbits

In this paper, a control effort minimizing optimal station-keeping guidance is designed and implemented to regulate a spacecraft around an L1 quasi-halo orbit in the Sun–Earth–Moon elliptic four-body problem. The station-keeping guidance is formulated as a finite time, non-linear optimal control pro...

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Vydáno v:	Acta astronautica Ročník 188; s. 518 - 530
Hlavní autoři:	Vutukuri, Srianish, Padhi, Radhakant
Médium:	Journal Article
Jazyk:	angličtina
Vydáno:	Elmsford Elsevier Ltd 01.11.2021 Elsevier BV
Témata:	Algorithms Circular restricted three body problem Constraint modelling Cost function Elliptic four body problem Four body problem Iterative methods Maneuvers Model predictive static programming Nonlinear control Optimal control Optimization Quasi-halo orbits Spacecraft Spacecraft guidance Station-keeping Terminal constraints Circular restricted three body problem Elliptic four body problem Quasi-halo orbits Station-keeping Model predictive static programming
ISSN:	0094-5765, 1879-2030
On-line přístup:	Získat plný text
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