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Journal: Applied SciencesVolume: 9Number: 5113
Article: Attitude Control in Ascent Phase of Missile Considering Actuator Non-Linearity and Wind Disturbance
  • Authors:
  • Bangsheng Fu1,2,
  • Hui Qi1 and
  • Jiangtao Xu1,*
  • et al.
Link: https://www.mdpi.com/2076-3417/9/23/5113

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