Optimal Powered Aerogravity-Assist Trajectories
Y Qi, A de Ruiter - Journal of Guidance, Control, and Dynamics, 2021 - arc.aiaa.org
THE gravity assist (GA) is a classical technique to change the path and energy of a
spacecraft flying close to a celestial body, which only needs gravitational forces from …
spacecraft flying close to a celestial body, which only needs gravitational forces from …
[HTML][HTML] Studying direct and indirect effects of impulses in powered aero-gravity-assist maneuvers around Venus
The study of aero-gravity-assisted maneuvers around Venus is the focus of the present
paper. These are maneuvers that combine the passage by the gravity field of the planet with …
paper. These are maneuvers that combine the passage by the gravity field of the planet with …
A survey on extensions of the pure gravity swing-by maneuver
The present paper surveys the more recent techniques related to the swing-by maneuver,
where a spacecraft changes its energy and angular momentum by passing close to celestial …
where a spacecraft changes its energy and angular momentum by passing close to celestial …
Application of Impulsive Aero-Gravity Assisted Maneuvers in Venus and Mars to Change the Orbital Inclination of a Spacecraft
JO Murcia-Piñeros, AFBA Prado - The Journal of the Astronautical …, 2019 - Springer
Thse powered aero-gravity-assist is an orbital maneuver that combines three basic
components: a gravity-assist with a passage by the atmosphere of the planet during the …
components: a gravity-assist with a passage by the atmosphere of the planet during the …
Effects of Bank Angle During Powered Aerogravity-Assist Maneuver
JOM Piñeros, AFBA Prado - Journal of Spacecraft and Rockets, 2021 - arc.aiaa.org
In a swing-by maneuver, the variation of energy of the spacecraft is controlled by the angle,
velocity, and distance of approach. These parameters are defined by the incoming trajectory …
velocity, and distance of approach. These parameters are defined by the incoming trajectory …
On the use of a continuous thrust to find bounded planar trajectories at given altitudes in Low Earth Orbits
In this work, it is shown how a spacecraft equipped with a thrust and subjected to a drag
force can be bounded at specific altitudes as function of the parameters of the thrust. It is …
force can be bounded at specific altitudes as function of the parameters of the thrust. It is …
Effects of the rotation of a spacecraft in an atmospheric close approach with the Earth
A maneuver called “Aerogravity Assisted” is known in the literature to increase the energy
gains given by a close approach between a spacecraft and a planet using the atmosphere of …
gains given by a close approach between a spacecraft and a planet using the atmosphere of …