2021
DOI: 10.3390/aerospace8120380
|View full text |Cite
|
Sign up to set email alerts
|

Prediction and Validation of Landing Stability of a Lunar Lander by a Classification Map Based on Touchdown Landing Dynamics’ Simulation Considering Soft Ground

Abstract: In this paper, a method for predicting the landing stability of a lunar lander by a classification map of the landing stability is proposed, considering the soft soil characteristics and the slope angle of the lunar surface. First, the landing stability condition in terms of the safe (=stable), sliding (=unstable), and tip-over (=statically unstable) possibilities was checked by dropping a lunar lander onto flat lunar surfaces through finite-element (FE) simulation according to the slope angle, friction coeffi… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1

Citation Types

0
0
0

Year Published

2022
2022
2024
2024

Publication Types

Select...
5

Relationship

0
5

Authors

Journals

citations
Cited by 5 publications
(3 citation statements)
references
References 30 publications
0
0
0
Order By: Relevance
“…In the drag force, ρ g is the plume gas density, u is the relative velocity u = (u g u p ), C D is the coefficient of drag (for a rough sphere, range between 0.3 and 0.6), and A p is the cross-sectional area of the particle. In the frictional force, µ is the coefficient of friction [34] and g is the acceleration of gravity on the Moon. To estimate the particle mass, we use the regolith particle density, ρ p , and volume.…”
Section: Velocity and Energy Rangementioning
confidence: 99%
“…In the drag force, ρ g is the plume gas density, u is the relative velocity u = (u g u p ), C D is the coefficient of drag (for a rough sphere, range between 0.3 and 0.6), and A p is the cross-sectional area of the particle. In the frictional force, µ is the coefficient of friction [34] and g is the acceleration of gravity on the Moon. To estimate the particle mass, we use the regolith particle density, ρ p , and volume.…”
Section: Velocity and Energy Rangementioning
confidence: 99%
“…When a lander is on its mission during a soft landing process, the surface irregularity of the target may have a significant influence on the landing dynamic performance [41,42]. In particular, the first points of contact usually occur between small rocks and the footpad's bottom surface, for which non-uniform compression is suspected throughout the landing process.…”
Section: Topology Optimization Of a Footpad Subjected To Impact Loadmentioning
confidence: 99%
“…The logistic regression: The statistical method can be used to model the probability of occurrence using the variables from the risk matrix and to predict the risk of error creation in new harnesses assessment [24].…”
mentioning
confidence: 99%