TY - GEN
T1 - The Design of Aerostat Platform System's Parameters Which Is Launched Form A Ballistic Missile
AU - Bai, Yunfei
AU - Kang, Rui
AU - Gao, Yeye
AU - Fu, Wenxing
N1 - Publisher Copyright:
© 2018 IEEE.
PY - 2018/8
Y1 - 2018/8
N2 - The stratospheric aerostat has higher use value, which is a hotspot of the near space development at home and abroad. In this paper, We will proposed fast deployment of aerostat which is focus on the stratospheric airship traditional deployment problems. We will go through the missile launch vehicle will be deployed to a predetermined airspace on the platform, and complete the rapid deployment of floating platform. The overall design of the rapid deployment of aerostat platform mainly completed in this paper, including, first, the design of aerostat airship shape; second, to determine the charging mechanism design of Aerostat Reducer; third, calculating parameters. Through the above three parts, we can design the Missile Ejection aerostat platform parameters, thus completing the overall design of the aerostat platform.
AB - The stratospheric aerostat has higher use value, which is a hotspot of the near space development at home and abroad. In this paper, We will proposed fast deployment of aerostat which is focus on the stratospheric airship traditional deployment problems. We will go through the missile launch vehicle will be deployed to a predetermined airspace on the platform, and complete the rapid deployment of floating platform. The overall design of the rapid deployment of aerostat platform mainly completed in this paper, including, first, the design of aerostat airship shape; second, to determine the charging mechanism design of Aerostat Reducer; third, calculating parameters. Through the above three parts, we can design the Missile Ejection aerostat platform parameters, thus completing the overall design of the aerostat platform.
KW - Aerostat Platform
KW - Parameters estimation
KW - Platform design
KW - Stratosphere
UR - http://www.scopus.com/inward/record.url?scp=85082459986&partnerID=8YFLogxK
U2 - 10.1109/GNCC42960.2018.9019106
DO - 10.1109/GNCC42960.2018.9019106
M3 - 会议稿件
AN - SCOPUS:85082459986
T3 - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
BT - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
Y2 - 10 August 2018 through 12 August 2018
ER -