北京航空航天大学主页平台系统 Wang Qing--英文主页-- Gong L, Wang Q, Dong C, Spacecraft output feedback attitude control based on extended state observer and adaptive dynamic programming[J]. Journal of the Franklin Institute, https://doi.org/10.1016/j.jfranklin.2019.04.018

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Gong L, Wang Q, Dong C, Spacecraft output feedback attitude control based on extended state observer and adaptive dynamic programming[J]. Journal of the Franklin Institute, https://doi.org/10.1016/j.jfranklin.2019.04.018

Release time:2019-08-29 Hits:

Translation or Not:no

Date of Publication:2019-08-30

Pre One:Zhang S, Wang Q, Dong C. Extended state observer based control for generic hypersonic vehicles with nonaffine-in-control character[J]. ISA transactions, 2018, 80: 27-36.

Next One:Gong L, Wang Q, Dong C, Disturbance rejection control of morphing aircraft based on switched nonlinear systems[J]. Nonlinear Dynamics, 2019, 92(2):975-995.

Wang Qing

Gender:Female Education Level:博士研究生 Alma Mater:西北工业大学 Degree:博士 Status:Employed School/Department:自动化科学与电气工程学院 Business Address:新主楼 E1109 Contact Information:010-82338161 E-Mail:

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Gong L, Wang Q, Dong C, Spacecraft output feedback attitude control based on extended state observer and adaptive dynamic programming[J]. Journal of the Franklin Institute, https://doi.org/10.1016/j.jfranklin.2019.04.018