A new method to identify the mass parameters of spacecraft
Abstract: 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.
- Standort
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Deutsche Nationalbibliothek Frankfurt am Main
- Umfang
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Online-Ressource
- Sprache
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Englisch
- Erschienen in
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A new method to identify the mass parameters of spacecraft ; volume:29 ; number:1 ; year:2020 ; pages:107-123 ; extent:17
Open astronomy ; 29, Heft 1 (2020), 107-123 (gesamt 17)
- Urheber
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Meng, Dongbo
Li, Xia
Pang, Jianguo
Lu, Jianxin
- DOI
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10.1515/astro-2020-0011
- URN
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urn:nbn:de:101:1-2405281620000.883564629356
- Rechteinformation
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Open Access; Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Letzte Aktualisierung
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14.08.2025, 10:55 MESZ
Datenpartner
Deutsche Nationalbibliothek. Bei Fragen zum Objekt wenden Sie sich bitte an den Datenpartner.
Beteiligte
- Meng, Dongbo
- Li, Xia
- Pang, Jianguo
- Lu, Jianxin