Searching for Orbits with Minimum Fuel Consumption for Station‐Keeping Maneuvers: An Application to Lunisolar Perturbations

AFBA Prado - Mathematical Problems in Engineering, 2013 - Wiley Online Library
The present paper has the goal of developing a new criterion to search for orbits that
minimize the fuel consumption for station‐keeping maneuvers. This approach is based on …

Onboard and Real‐Time Artificial Satellite Orbit Determination Using GPS

APM Chiaradia, HK Kuga… - … Problems in Engineering, 2013 - Wiley Online Library
An algorithm for real‐time and onboard orbit determination applying the Extended Kalman
Filter (EKF) method is developed. Aiming at a very simple and still fairly accurate orbit …

[PDF][PDF] Resonant Orbits for the Space Debris

JKS Formiga, DPS Santos… - International Journal of …, 2019 - academia.edu
The present paper has the goal of studying the changes of the orbital parameters
considering a fragment that makes a close approach with the Saturn. Successive swing-by …

[PDF][PDF] Three-dimensional two-impulsive orbital maneuvers with time limit

EM Rocco, A Prado, MLO Souza - WSEAS Transactions on …, 2013 - plutao.dpi.inpe.br
The problem of three-dimensional two-impulsive orbital maneuvers between two elliptical
orbits with minimum fuel consumption, but having a time limit, is considered in the present …

The study of the asymmetric multiple encounters problem and its application to obtain Jupiter gravity assisted maneuvers

DPS dos Santos, AFB de Almeida Prado… - Mathematical …, 2013 - Wiley Online Library
The Multiple Encounters Problem is described in the literature as the problem of finding
trajectories for a spacecraft that leaves from a mother planet, describes a trajectory in the …

[PDF][PDF] Embedded Spaces of Hermite Splines

YK Dem'yanovich, IG Burova, TO Evdokimova… - … on Applied and …, 2019 - wseas.com
This paper is devoted to the processing of large numerical signals which arise in different
technical problems (for example, in positioning systems, satellite maneuvers, in the …

[PDF][PDF] Research Article The Study of the Asymmetric Multiple Encounters Problem and Its Application to Obtain Jupiter Gravity Assisted Maneuvers

Research Article The Study of the Asymmetric Multiple Encounters Problem and Its
Application to Obtain Jupiter Gravity Assisted Page 1 Hindawi Publishing Corporation …

[PDF][PDF] Determination of onboard coplanar orbital maneuvers with orbits determined using GPS

APM Chiaradia, AFBA Prado, HK Kuga - WSEAS Transactions on Applied …, 2012 - Citeseer
In the present paper a study is made in order to find an algorithm that can calculate coplanar
orbital maneuvers for an artificial satellite. The idea is to find a method that is fast enough to …