Abstract：Morphing aircraft can achieve better performance by changing the aerodynamic shape in different flying tasks or various tasks of the same task stage. Telescopic wings are one of the important deformation schemes for aircraft. In order to improving design accuracy and development efficiency, the co-simulation approach has been paid great attention recently. The co-simulation method can verify the influence of parameters on the performance of Telescopic wings during the design phase.Using ADAMS and Simulink,a comprehensive analysis and simulation mechatronic model had been established to study the kinematic and the dynamic characteristics. To meet the standards of real-time deployment of the deformation mechanism, the main parameters of the deformation wing mechanism were simulated and ameliorated. The simulation experimenthas verified the feasibility of the proposed method and provide a foundation for structural optimization design.
许泉, 周丽, 徐胜利, 陆丰玮, 刘思禹, 刘广, 华洲. 变体飞行器伸缩翼机构设计与仿真[J]. 空天防御, 2023, 6(2): 35-42.
XU Quan, ZHOU Li, XU Shengli, LU Fengwei, LIU Siyu, LIU Guang, Hua Zhou . Design and Simulation for the Telescopic Wing of Morphing Aircraft. Air & Space Defense, 2023, 6(2): 35-42.
