TY - JOUR
T1 - Influence of the Lander Size and Shape on the Ballistic Landing Motion
AU - Zeng, X. Y.
AU - Li, Z. W.
AU - Wen, T. G.
AU - Zhang, Y. L.
N1 - Publisher Copyright:
© 2022 The Authors. Earth and Space Science published by Wiley Periodicals LLC on behalf of American Geophysical Union.
PY - 2022/2
Y1 - 2022/2
N2 - This article investigates the ballistic landing motion and final distribution of the landers in different sizes or shapes near the small celestial body. Three typical shapes, including cubic, cuboid, and cylindrical, are considered for the landers deployed to a tri-axial ellipsoid model. The Polygonal Contact Model (PCM) is used to detect the contact/collision, where the Hertz model is applied to calculate the continuous contact force. Different-sized cubic landers (in the edge length of 20, 30, 40, and 50 cm) are numerically simulated to examine how the lander size influences its dynamics. The landing motion of the cuboid- and the cylinder-shaped landers are then analyzed in the same technique. The heights of these asymmetrical landers are assumed to be 25, 30, and 35 cm, respectively, to illustrate the shape effect. Monte Carlo simulations are implemented for various landers to account for the surface motion randomness. The final dispersion, the outgoing velocity after the collision, the horizontal transfer distance, and the settling time are taken to be critical indicators for discussing the landing behavior, which can provide implications for the probe design of future missions.
AB - This article investigates the ballistic landing motion and final distribution of the landers in different sizes or shapes near the small celestial body. Three typical shapes, including cubic, cuboid, and cylindrical, are considered for the landers deployed to a tri-axial ellipsoid model. The Polygonal Contact Model (PCM) is used to detect the contact/collision, where the Hertz model is applied to calculate the continuous contact force. Different-sized cubic landers (in the edge length of 20, 30, 40, and 50 cm) are numerically simulated to examine how the lander size influences its dynamics. The landing motion of the cuboid- and the cylinder-shaped landers are then analyzed in the same technique. The heights of these asymmetrical landers are assumed to be 25, 30, and 35 cm, respectively, to illustrate the shape effect. Monte Carlo simulations are implemented for various landers to account for the surface motion randomness. The final dispersion, the outgoing velocity after the collision, the horizontal transfer distance, and the settling time are taken to be critical indicators for discussing the landing behavior, which can provide implications for the probe design of future missions.
KW - asteroid surface exploration
KW - lander size and shape
KW - trajectory evolution
UR - http://www.scopus.com/inward/record.url?scp=85125150728&partnerID=8YFLogxK
U2 - 10.1029/2021EA001952
DO - 10.1029/2021EA001952
M3 - Article
AN - SCOPUS:85125150728
SN - 2333-5084
VL - 9
JO - Earth and Space Science
JF - Earth and Space Science
IS - 2
M1 - e2021EA001952
ER -