Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Zhouhui Tuo"'
Publikováno v:
Acta Astronautica. 131:159-165
Ever-increasing launch of small satellites demands an effective and efficient computer-aided analysis approach to shorten the ground test cycle and save the economic cost. However, the multiple influencing factors hamper the efficiency and accuracy o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::88515229b5890bbbdfd441dfd2f30703
https://doi.org/10.1016/j.actaastro.2016.10.042
https://doi.org/10.1016/j.actaastro.2016.10.042
Publikováno v:
Advances in Structural and Multidisciplinary Optimization ISBN: 9783319679877
The increasing demand for greater satellite mission capabilities has led to the need for lighter, stronger space deployable structures within the limited packaged volume. Tubular extendable booms, characterized by small stowed volume, light weight an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4e9224c550d67a052c78096834540c82
https://doi.org/10.1007/978-3-319-67988-4_46
https://doi.org/10.1007/978-3-319-67988-4_46
Publikováno v:
Acta Astronautica. 102:151-155
Elastic launch devices are widely used in aviation and aerospace, whereas the accurate assessment and practical control of their dynamic performance are often complicated. We propose and validate a metric approach to simplify the launch dynamics, reg
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::78672956be1c4889d36fca55842ad765
https://doi.org/10.1016/j.actaastro.2014.05.028
https://doi.org/10.1016/j.actaastro.2014.05.028
Publikováno v:
Science China Earth Sciences. 56:2198-2208
China has developed an airborne gravimetry system based on SINS/DGPS named SGA-WZ, the first system in which a strapdown inertial navigation system (SINS) has been used for airborne gravimetry in China. This gravity measurement system consists of a s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::02134916bbdf19f76efd59edd3f7adad
https://doi.org/10.1007/s11430-013-4726-y
https://doi.org/10.1007/s11430-013-4726-y
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 227:1968-1976
The separation system is crucial for the launch of satellites. Dynamic characteristics of satellite separation are quite complex and difficult to predict. With respect to the helical compression spring mechanism, an approach using transient perturbat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4e25718e934e670221c999d580299613
https://doi.org/10.1177/0954410012466780
https://doi.org/10.1177/0954410012466780
Publikováno v:
2008 International Conference on Information and Automation.
The spatial domain imaging model of micro-zooming is established. According to the model, the relationship between observed images and ideal high resolution image is given as a set of large, sparse and inconsistent linear equations. And the high reso
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ed7b10e224b7ebf194fca013562fee1b
https://doi.org/10.1109/icinfa.2008.4607974
https://doi.org/10.1109/icinfa.2008.4607974
Publikováno v:
Fifth International Symposium on Instrumentation and Control Technology.
A shipboard attitude reference and control system using fiber optic gyros is analyzed. In this system, the frequency character of the attitude error is more concerned, because high frequency attitude measuring errors can some times cause vibration in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::87d2afd059e8bf90953656c96055bc42
https://doi.org/10.1117/12.522345
https://doi.org/10.1117/12.522345
Autor:
Xingzhi Hu1 huxingzhi@nudt.edu.cn, Xiaoqian Chen1 chenxiaoqian@nudt.edu.cn, Zhouhui Tuo1, Yong Zhao1
Publikováno v:
Acta Astronautica. Sep2014, Vol. 102, p151-155. 5p.