most citedA Circular Restricted n-body Problem

10 citations · 16 across the 4 of their papers we have counts for

collaborators

6 papers

eess.SY20236 cited

Autonomous and Robust Orbit-keeping for Small Body Missions

Rodolfo Batista Negri, Antonio Fernando Bertachini de Almeida Prado

This article presents a path-following control law for autonomous orbital maintenance of small body missions. The control law is robust, stable, and capable of controlling only the…

eess.SY202310 cited

A Circular Restricted n-body Problem

Rodolfo Batista Negri, Antonio Fernando Bertachini de Almeida Prado

This paper introduces the Circular Restricted n-Body Problem (CRNBP), an extension of the bicircular restricted four-body problem (BCR4BP) designed to describe the dynamics of an n…

astro-ph.EP2023

Parametric Optimization of Low Thrust Orbital Maneuvers

Antonio Fernando Bertachini de Almeida Prado

The goal of the present paper is to make a numerical analysis of parametric optimization of low thrust orbital maneuver. An orbital maneuver occurs when it is necessary to modify t…

astro-ph.EP2023

Study on Autonomous Gravity-assists with a Path-following Control

Rodolfo Batista Negri, Antônio Fernando Bertachini de Almeida Prado

We investigate the autonomous control of gravity-assist hyperbolic trajectories using a path following control law based on sliding mode control theory. This control strategy ensur…

math.DS2023

Using low Lift-to-Drag spacecraft to perform upper atmospheric Aero-Gravity Assisted Maneuvers

Jhonathan O. Murcia Piñeros, Rodolpho Vilhena de Moraes, Antônio F. Bertachini de Almeida Prado

The Gravity Assisted Maneuver has been applied in lots of space missions, to change the spacecraft heliocentric velocity vector and the geometry of the orbit, after the close appro…

astro-ph.EP2023

Applying the perturbative integral in aeromaneuvers around Mars to calculate the cost

Jhonathan O. Murcia Piñeros, Antônio F. Bertachini de Almeida Prado, Walter Abrahão dos Santos +1

The perturbative integral method was applied to quantify the contribution of external forces during a specific interval of time in trajectories of spacecraft around asteroids and u…