A new method to identify the mass parameters of spacecraft

A two-step identification method is proposed, both the moment of inertia and the mass properties are identified. A new index parameter which is different from the commonly used condition number is first defined for designing the optimal excitation. A method is introduced based on the least squares a...

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Bibliographic Details
Main Authors: Meng Dongbo, Li Xia, Pang Jianguo, Lu Jianxin
Format: Article
Language:English
Published: De Gruyter 2020-10-01
Series:Open Astronomy
Subjects:
Online Access:https://doi.org/10.1515/astro-2020-0011
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spelling doaj-465445d72b1945308ace3a28323049742021-09-06T19:40:15ZengDe GruyterOpen Astronomy2543-63762020-10-0129110712310.1515/astro-2020-0011astro-2020-0011A new method to identify the mass parameters of spacecraftMeng Dongbo0Li Xia1Pang Jianguo2Lu Jianxin3School of Aerospace Engineering, Tsinghua University, Tsinghua University, Beijing, China, 100084; Taiyuan Satellite Launch Center, Taiyuan, Shanxi, China, 030027; Email:Shanxi Technology and Business College,Taiyuan, Shanxi, China, 030006Taiyuan Satellite Launch Center,Taiyuan, Shanxi, China, 030027Taiyuan Satellite Launch Center,Taiyuan, Shanxi, China, 030027A two-step identification method is proposed, both the moment of inertia and the mass properties are identified. A new index parameter which is different from the commonly used condition number is first defined for designing the optimal excitation. A method is introduced based on the least squares algorithm. Detailed mathematical equations and numerical analysis are proposed. Simulation results show that the proposed method can identify the mass parameters of spacecraft.https://doi.org/10.1515/astro-2020-0011mass parametersinertiaidentificationcondition numberoptimal excitation
collection DOAJ
language English
format Article
sources DOAJ
author Meng Dongbo
Li Xia
Pang Jianguo
Lu Jianxin
spellingShingle Meng Dongbo
Li Xia
Pang Jianguo
Lu Jianxin
A new method to identify the mass parameters of spacecraft
Open Astronomy
mass parameters
inertia
identification
condition number
optimal excitation
author_facet Meng Dongbo
Li Xia
Pang Jianguo
Lu Jianxin
author_sort Meng Dongbo
title A new method to identify the mass parameters of spacecraft
title_short A new method to identify the mass parameters of spacecraft
title_full A new method to identify the mass parameters of spacecraft
title_fullStr A new method to identify the mass parameters of spacecraft
title_full_unstemmed A new method to identify the mass parameters of spacecraft
title_sort new method to identify the mass parameters of spacecraft
publisher De Gruyter
series Open Astronomy
issn 2543-6376
publishDate 2020-10-01
description A two-step identification method is proposed, both the moment of inertia and the mass properties are identified. A new index parameter which is different from the commonly used condition number is first defined for designing the optimal excitation. A method is introduced based on the least squares algorithm. Detailed mathematical equations and numerical analysis are proposed. Simulation results show that the proposed method can identify the mass parameters of spacecraft.
topic mass parameters
inertia
identification
condition number
optimal excitation
url https://doi.org/10.1515/astro-2020-0011
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