Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Qibo Peng"'
Publikováno v:
Applied Sciences, Vol 13, Iss 9, p 5419 (2023)
System-of-systems (SoS) architecture is crucial in managing complex and interconnected systems. However, the description and modeling of SoS architecture pose significant challenges and require a structured and organized approach. In this study, a me
Externí odkaz:
https://doaj.org/article/d983f80ca227435a8c070d40c9f1bc63
Publikováno v:
Applied Sciences, Vol 12, Iss 17, p 8716 (2022)
The exploration of the Moon has always been a hot topic. The determination of the Moon-to-Earth transfer opportunity and the design of the precise transfer trajectory play important roles in manned Moon exploration missions. It is still a difficult p
Externí odkaz:
https://doaj.org/article/31d6d07987404f2889ec5128381463b3
Publikováno v:
Aerospace, Vol 9, Iss 4, p 182 (2022)
We propose two approaches based on feedforward control and model-predictive control, respectively, to solve the station-keeping problem of an electric-propulsion geostationary Earth orbit (GEO) satellite, whose thrusters are mounted on two robotic ar
Externí odkaz:
https://doaj.org/article/7e35227ebf164db0a5e2e3df9d2a29d7
Publikováno v:
Acta Astronautica. 199:125-133
Publikováno v:
Acta Astronautica.
Publikováno v:
Reliability Engineering & System Safety. 229:108866
Publikováno v:
Acta Astronautica. 160:365-377
This study proposes a high-precision fixed-thrust free return orbit design method for a manned lunar mission centred on the rendezvous and docking with the lunar space station. Future manned lunar landing missions based on the lunar space station wil
Publikováno v:
Science China Technological Sciences. 55:2561-2569
Publikováno v:
Science China Technological Sciences. 54:3243-3250
Point return orbit (PRO) of manned lunar mission is constrained by both lunar parking orbit and reentry corridor associated with reentry position. Besides, the fuel consumption and flight time should be economy. The patched conic equations which are
Autor:
Qibo Peng
Publikováno v:
Genetic Algorithms in Applications
Finite-thrust propulsion is now widely used in space missions, such as lunar or mars descent, interplanetary transfer, spacecraft rendezvous, etc.. The finite-thrust optimal control problem is qualitatively different from the impulsive case as there
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::58bb734aa714e4c7a22fc11279d3bd8f
http://www.intechopen.com/articles/show/title/finite-thrust-trajectory-optimization-using-a-combination-of-gauss-pseudospectral-method-and-genetic
http://www.intechopen.com/articles/show/title/finite-thrust-trajectory-optimization-using-a-combination-of-gauss-pseudospectral-method-and-genetic