Analysis and control for the mode transition of tandem-wing aircraft with variable sweep

HIGHLIGHTS

• who: Liang Gao et al. from the State Key Laboratory of Robotics and System, Harbin Institute of Technology, Harbin, China have published the article: Analysis and Control for the Mode Transition of Tandem-Wing Aircraft with Variable Sweep, in the Journal: Aerospace 2022, 463 of /2022/
• what: In this paper, an innovative morphing scheme is investigated to weaken the additional inertia forces and moments caused by morphing.
• how: In this paper the Jacobian linearization approach is used to obtain the LPV model of the variable sweep MAV. By combining and_(9) the LPV . . .
  

   

  

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