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Journal: AerospaceVolume: 10Number: 696
Article: Flight Tracking Control for Helicopter Attitude and Altitude Systems Using Output Feedback Method under Full State Constraints
  • Authors:
  • Yankai Li1,2,*,†,
  • Yulong Huang1,† and
  • Dongping Li3,*
  • et al.
Link: https://www.mdpi.com/2226-4310/10/8/696

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