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Journal: Appl. Sci., 2019
Volume: 9
Number: 5113
Article:
Attitude Control in Ascent Phase of Missile Considering Actuator Non-Linearity and Wind Disturbance
Authors:
by
Bangsheng Fu, Hui Qi, Jiangtao Xu, Ya Yang, Shaobo Wang and Quanxi Gao
Link:
https://www.mdpi.com/2076-3417/9/23/5113
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