Computer Science

Computer Science ›› 2020, Vol. 47 ›› Issue (11A): 651-656.doi: 10.11896/jsjkx.200100026

• Interdiscipline & Application • Previous Articles     Next Articles

Fast Design and Verification of Flight Control Law for Small Compound UAV

TAN Si-yang   

  1. AVIC Digital Co.,Ltd,Beijing 100028,China
  • Online:2020-11-15 Published:2020-11-17
  • About author:TAN Si-yang,born in 1991,master.Her main research interests include systemsimulation,model-based control system design and simulation.

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Abstract: With the in-depth study of VTOL aircraft,the design of its flight control law has gradually become the focus of research.The rapid design and verification method of the flight control law of small compound UAV is studied.First,a small compound VTOL aircraft layout is proposed.Then,the mission profile is set up and the flight control law is designed based on it.The model of flight control law is built based on MATLAB/Simulink platform while the model of aircraft ontology is built based on Amesim platform.The flight control law algorithm is validated by modeling and simulation,and the fast iterative optimization of flight control law design scheme is realized by analyzing flight performance simulation results.Meantime,the fast design and verification solution can be used as a reference for the joint simulation and analysis of control systems and controlled objects in other aerospace fields.

Key words: Compound Aircraft, Fixed wing, Four rotor, Modeling, Simulation

CLC Number: 

  • V249
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