Prediction of Orbit Decay for Large-Scale Spacecraft considering Rarefied Aerodynamic Perturbation Effects
The growing risk of falling debris from outer space as well as the atmospheric interaction effect makes the orbit decay prediction of large spacecraft in very low earth orbit (VLEO) increasingly significant. Focusing on the aerodynamic perturbation effects under multiscale and nonequilibrium states...
Saved in:
Main Authors: | Xinglong Gao, Zhihui Li, Qin Chen, Di Ding, Aoping Peng |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2022-01-01
|
Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2022/8984056 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Investigation of Aerodynamic Characteristics of Aircrafts in a Rarefied Gas Flow Using the Moment Method
by: Auzhan Sakabekov, et al.
Published: (2022-01-01) -
Coupling Dynamic Behavior Characteristics of a Spacecraft Beam with Composite Laminated Structures and Large-Scale Motions
by: Bindi You, et al.
Published: (2018-01-01) -
Expandable Orbit Decay Prediction Using Continual Learning
by: Junhua He, et al.
Published: (2024-01-01) -
Finite-Time Orbit Control for Spacecraft Formation with External Disturbances and Limited Data Communication
by: Lei Xing, et al.
Published: (2022-01-01) -
Aerodynamic Design and Performance Analysis of a Large-Scale Composite Blade for Wind Turbines
by: Semyoung Lim, et al.
Published: (2025-01-01)