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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Online Access: | https://doi.org/10.1515/astro-2020-0011 |
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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 |
work_keys_str_mv |
AT mengdongbo anewmethodtoidentifythemassparametersofspacecraft AT lixia anewmethodtoidentifythemassparametersofspacecraft AT pangjianguo anewmethodtoidentifythemassparametersofspacecraft AT lujianxin anewmethodtoidentifythemassparametersofspacecraft AT mengdongbo newmethodtoidentifythemassparametersofspacecraft AT lixia newmethodtoidentifythemassparametersofspacecraft AT pangjianguo newmethodtoidentifythemassparametersofspacecraft AT lujianxin newmethodtoidentifythemassparametersofspacecraft |
_version_ |
1717769002307026944 |