Solar sail-based V-infinity leveraging missions from elliptic orbit

AA Quarta, C Bianchi, L Niccolai, G Mengali - Aerospace Science and …, 2022 - Elsevier
The utilization of V∞ leveraging maneuvers in deep space missions is able to mitigate the
mission requirements on launch energy, as the spacecraft propulsive acceleration is used to …

Tether System in Martian-Moons-eXploration-Like Mission for Phobos Surface Exploration

VS Aslanov - Journal of Spacecraft and Rockets, 2024 - arc.aiaa.org
IN THE last half-century, the field of space tether systems has attracted much attention; and
this is reflected in several books (eg, Refs.[1–3]) and in hundreds of papers (eg, Refs.[4 …

B–plane assisted trajectory design with analytical mapping of swing-by parameters

T Chikazawa, Y Kawakatsu - Advances in Space Research, 2024 - Elsevier
The Artemis program has gathered further attention due to the transfer trajectories to the
Moon and beyond. Trajectories such as weak stability boundary and ballistic lunar transfer …

Optimal Earth Gravity-Assist Maneuvers with an Electric Solar Wind Sail

L Niccolai, M Bassetto, AA Quarta, G Mengali - Aerospace, 2022 - mdpi.com
Propellantless propulsive systems such as Electric Solar Wind Sails are capable of
accelerating a deep-space probe, only requiring a small amount of propellant for attitude …

Robust trajectory optimization with chance-constrained formulation

N Marmo - 2024 - tesidottorato.depositolegale.it
This thesis investigates the chance-constraint formulation of robust trajectory optimization for
space applications. The importance of robustness in space trajectory optimization is growing …

火星衛星探査計画MMX の軌道設計

尾崎直哉, 井上博夏, 尾川順子, 池田人, バレシニコラ… - jxiv.jst.go.jp
抄録 火星衛星探査計画 MMX は, 2020 年代に打ち上げられる JAXA の戦略的中型ミッションで
ある. MMX は火星の衛星を探査し, フォボスからサンプルを回収して地球に持ち帰る. 本論文では …