火星伞降段多体动力学特性分析与安全设计研究

Jie Dong; Wei Rao; Ze Zhou Sun; Chuang Wang; Guo Qiang Liu; Hu Tao Cui; Yang Tian; Jian Li; Yan Wang

doi:10.1360/SST-2022-0002

火星伞降段多体动力学特性分析与安全设计研究

Translated title of the contribution: Multibody dynamics characteristics analysis and safety design research of the Mars parachute descent process

Jie Dong^*
, Wei Rao
, Ze Zhou Sun
, Chuang Wang
, Guo Qiang Liu
, Hu Tao Cui
, Yang Tian
, Jian Li
, Yan Wang

^*Corresponding author for this work

China Aerospace Science and Technology Corporation
School of Astronautics, Harbin Institute of Technology

Research output: Contribution to journal › Article › peer-review

4 Scopus citations

Abstract

This paper focuses on solving the technical challenges brought by the multibody movement during the Mars parachute deceleration stage. First, the parachute system’s design scheme is introduced. The mechanism and main effects of the dynamic characteristics of the parachute deceleration process are analyzed using simulations and typical experiments. Then, the safety design schemes for parachutes, separation of heatshield, autonomous navigation, and attitude control are proposed. Finally, the in-flight results of Tianwen-1’s parachute descent process are introduced. This research can provide a meaningful reference for subsequent Mars landing missions.

Translated title of the contribution	Multibody dynamics characteristics analysis and safety design research of the Mars parachute descent process
Original language	Chinese (Traditional)
Pages (from-to)	1175-1185
Number of pages	11
Journal	Scientia Sinica Technologica
Volume	52
Issue number	8
DOIs	https://doi.org/10.1360/SST-2022-0002
State	Published - 2022
Externally published	Yes

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title = "火星伞降段多体动力学特性分析与安全设计研究",

abstract = "This paper focuses on solving the technical challenges brought by the multibody movement during the Mars parachute deceleration stage. First, the parachute system{\textquoteright}s design scheme is introduced. The mechanism and main effects of the dynamic characteristics of the parachute deceleration process are analyzed using simulations and typical experiments. Then, the safety design schemes for parachutes, separation of heatshield, autonomous navigation, and attitude control are proposed. Finally, the in-flight results of Tianwen-1{\textquoteright}s parachute descent process are introduced. This research can provide a meaningful reference for subsequent Mars landing missions.",

keywords = "Mars, Tianwen-1, dynamics characteristics, parachute",

author = "Jie Dong and Wei Rao and Sun, \{Ze Zhou\} and Chuang Wang and Liu, \{Guo Qiang\} and Cui, \{Hu Tao\} and Yang Tian and Jian Li and Yan Wang",

year = "2022",

doi = "10.1360/SST-2022-0002",

language = "繁体中文",

volume = "52",

pages = "1175--1185",

journal = "Scientia Sinica Technologica",

issn = "1674-7259",

publisher = "Science Press ",

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T1 - 火星伞降段多体动力学特性分析与安全设计研究

AU - Dong, Jie

AU - Rao, Wei

AU - Sun, Ze Zhou

AU - Wang, Chuang

AU - Liu, Guo Qiang

AU - Cui, Hu Tao

AU - Tian, Yang

AU - Li, Jian

AU - Wang, Yan

PY - 2022

Y1 - 2022

N2 - This paper focuses on solving the technical challenges brought by the multibody movement during the Mars parachute deceleration stage. First, the parachute system’s design scheme is introduced. The mechanism and main effects of the dynamic characteristics of the parachute deceleration process are analyzed using simulations and typical experiments. Then, the safety design schemes for parachutes, separation of heatshield, autonomous navigation, and attitude control are proposed. Finally, the in-flight results of Tianwen-1’s parachute descent process are introduced. This research can provide a meaningful reference for subsequent Mars landing missions.

AB - This paper focuses on solving the technical challenges brought by the multibody movement during the Mars parachute deceleration stage. First, the parachute system’s design scheme is introduced. The mechanism and main effects of the dynamic characteristics of the parachute deceleration process are analyzed using simulations and typical experiments. Then, the safety design schemes for parachutes, separation of heatshield, autonomous navigation, and attitude control are proposed. Finally, the in-flight results of Tianwen-1’s parachute descent process are introduced. This research can provide a meaningful reference for subsequent Mars landing missions.

KW - Mars

KW - Tianwen-1

KW - dynamics characteristics

KW - parachute

UR - https://www.scopus.com/pages/publications/85137705685

U2 - 10.1360/SST-2022-0002

DO - 10.1360/SST-2022-0002

M3 - 文章

AN - SCOPUS:85137705685

SN - 1674-7259

VL - 52

SP - 1175

EP - 1185

JO - Scientia Sinica Technologica

JF - Scientia Sinica Technologica

IS - 8

ER -

火星伞降段多体动力学特性分析与安全设计研究

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