Multiple Flybys of Venus Co-orbital Asteroids using Resonant Orbits and Gravity Assist Maneuvers

Flyby schemes for asteroids in orbital resonance with Venus are considered. The possibility of organizing multiple approaches of a spacecraft to such asteroids while moving along heliocentric orbits resonant with the orbit of Venus in a 1 : 1 ratio is demonstrated. Of the twenty known co-orbital asteroids, it was possible to flyby ten that are in short-term resonance orbits and periodically approach Venus. To circumvent the limitation associated with the complexity of momentum-free capture of a spacecraft into a permanent orbital resonance with a planet, combined schemes have been proposed. In these schemes, the spacecraft, with each approach to Venus, transitions between different resonant orbits, which allows it to alternate flybys of a co-orbital asteroid with approaches to near-Earth asteroids, including potentially hazardous ones. This approach ensures effective control of the spacecraft’s trajectory through gravity assist maneuvers and also increases the scientific significance of the mission as a whole.

Authors

Institutions

Publication Details

Journal
Solar System Research
Published
2026-03-23
DOI
https://doi.org/10.1134/s0038094625601367
Primary Topic
Spacecraft Dynamics and Control
Type
article
Field-Weighted Citation Impact
0.00
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

Multiple Flybys of Venus Co-orbital Asteroids using Resonant Orbits and Gravity Assist Maneuvers

O. S. Chernenko, M. V. Pupkov, V. A. Zubko, K. S. Fedyaev et al.
Solar System Research
Spacecraft Dynamics and Control
article

Multiple Flybys of Venus Co-orbital Asteroids using Resonant Orbits and Gravity Assist Maneuvers

O. S. Chernenko, M. V. Pupkov, V. A. Zubko, K. S. Fedyaev, N. A. Eismont
article en

Abstract

Flyby schemes for asteroids in orbital resonance with Venus are considered. The possibility of organizing multiple approaches of a spacecraft to such asteroids while moving along heliocentric orbits resonant with the orbit of Venus in a 1 : 1 ratio is demonstrated. Of the twenty known co-orbital asteroids, it was possible to flyby ten that are in short-term resonance orbits and periodically approach Venus. To circumvent the limitation associated with the complexity of momentum-free capture of a spacecraft into a permanent orbital resonance with a planet, combined schemes have been proposed. In these schemes, the spacecraft, with each approach to Venus, transitions between different resonant orbits, which allows it to alternate flybys of a co-orbital asteroid with approaches to near-Earth asteroids, including potentially hazardous ones. This approach ensures effective control of the spacecraft’s trajectory through gravity assist maneuvers and also increases the scientific significance of the mission as a whole.

Solar System ResearchVol. 60(2)
Space Research Institute (RU)
Openalex Percentile: Top 10%
Spacecraft Dynamics and Control
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.

Multiple Flybys of Venus Co-orbital Asteroids using Resonant Orbits and Gravity Assist Maneuvers — O. S. Chernenko, M. V. Pupkov, et al. · Solar System Research (2026) | TGRS Research Map | TGRS