Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Chen, Shuitian"'
Autor:
Zhao, Pengyue, Quan, Qiquan, Chen, Shuitian, Yang, Tingting, Bai, Deen, Tang, Dewei, Deng, Zongquan
Publikováno v:
In Acta Astronautica April 2019 157:300-309
Publikováno v:
In Aerospace Science and Technology March 2019 86:582-591
Publikováno v:
RCAR
This paper presents design of hover performance setups and preliminary experiments to validate the possibility of a miniature Mars rotorcraft's flying in Martian atmosphere. Conceptual design of the miniature Mars rotorcraft named MarsBird-I is propo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f61ef6db23b7de260ed5a479ec0180f8
https://doi.org/10.1109/rcar52367.2021.9517676
https://doi.org/10.1109/rcar52367.2021.9517676
Publikováno v:
Acta Astronautica. 157:300-309
Mars rotorcraft, as an aerial auxiliary platform can assist Mars rover to complete exploration missions, is of great significance in the field of planetary exploration. The complex terrain on Mars limits the working range of the Mars rover, whereas a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5cda7a1ff967f178a47136d2f0786c5b
https://doi.org/10.1016/j.actaastro.2018.12.026
https://doi.org/10.1016/j.actaastro.2018.12.026
Publikováno v:
2017 IEEE International Conference on Mechatronics and Automation (ICMA).
This paper presents a detailed experimental approach for understanding and optimizing the hover performance of Martian UAV rotor, including a systematic discussion about several coefficients for hover characteristics and a detailed design approach fo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::34974648ebf314beebfa1f9e1181ba45
https://doi.org/10.1109/icma.2017.8016118
https://doi.org/10.1109/icma.2017.8016118
Publikováno v:
2017 IEEE International Conference on Mechatronics and Automation (ICMA).
In order to verify whether a small-scale rotorcraft can fly on Mars, this paper is proposed to establish a Martian atmosphere simulator and to design a hover test stand for coaxial rotorcraft rotor. Since the ultra-low air density of Mars is approxim
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1ae3a468369ceb618ba6b70156c75a2f
https://doi.org/10.1109/icma.2017.8016026
https://doi.org/10.1109/icma.2017.8016026