Flyby schemes demonstrate effective trajectory control for spacecraft near Venus, suggesting enhanced mission potential.
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.
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Zubko et al. (2026) studied this question.
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