2014
DOI: 10.2478/arsa-2014-0006
|View full text |Cite
|
Sign up to set email alerts
|

From Tensor to Vector of Gravitation

Abstract: Different gravitational force models are used for determining the satellites' orbits. The satellite gravity gradiometry (SGG) data contain this gravitational information and the satellite accelerations can be determined from them. In this study, we present that amongst the elements of the gravitational tensor in the local north-oriented frame, all of the elements are suitable for this purpose except Txy. Three integral formulae with the same kernel function are presented for recovering the accelerations from t… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2

Citation Types

0
2
0

Year Published

2016
2016
2016
2016

Publication Types

Select...
1

Relationship

0
1

Authors

Journals

citations
Cited by 1 publication
(2 citation statements)
references
References 40 publications
0
2
0
Order By: Relevance
“…Bobojü and DroĪyner (2003) showed the possibility of using the gravity gradient tensor components to improve simulated low Earth-orbiting (LEO) satellite orbits. An interesting idea of the application of dynamical aspect of gravity gradients for a satellite orbit determination is given by Eshagh (2014). The satellite acceleration vector is derived from gravity gradients in order to determine an orbit by the numerical integration (Eshagh 2014).…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…Bobojü and DroĪyner (2003) showed the possibility of using the gravity gradient tensor components to improve simulated low Earth-orbiting (LEO) satellite orbits. An interesting idea of the application of dynamical aspect of gravity gradients for a satellite orbit determination is given by Eshagh (2014). The satellite acceleration vector is derived from gravity gradients in order to determine an orbit by the numerical integration (Eshagh 2014).…”
Section: Introductionmentioning
confidence: 99%
“…An interesting idea of the application of dynamical aspect of gravity gradients for a satellite orbit determination is given by Eshagh (2014). The satellite acceleration vector is derived from gravity gradients in order to determine an orbit by the numerical integration (Eshagh 2014).…”
Section: Introductionmentioning
confidence: 99%