CAJ | 학술논문

针对紧密编队飞行过程中产生的尾涡流场对空中加油机产生扰动影响的问题，建立了受油机扰动运动模型。将风扰动主要分解为大气紊流和加油机尾涡，分别建立工程化的Dryden大气紊流模型和尾涡模型，将叠加的2个扰动加入到受油机的非线性刚体运动方程中，并对受油机扰动运动进行仿真分析。仿真结果表明：该叠加的方法能够简单有效地模拟反映复杂的气流扰动，为进一步研究空中加油控制系统提供参考。
침대긴밀편대비행과정중산생적미와류장대공중가유궤산생우동영향적문제，건립료수유궤우동운동모형。장풍우동주요분해위대기문류화가유궤미와，분별건립공정화적Dryden대기문류모형화미와모형，장첩가적2개우동가입도수유궤적비선성강체운동방정중，병대수유궤우동운동진행방진분석。방진결과표명：해첩가적방법능구간단유효지모의반영복잡적기류우동，위진일보연구공중가유공제계통제공삼고。
Trailing vortex is come into being during the close formation flight, which will truly influence the aerial refueling. The receiver aircraft disturbance modeling is aimed for solving this problem. One account of the wind influence of both atmosphere disturbance and trailing vortex of tanker aircraft, the engineering Dryden atmospheric disturbance model and trailing vortex model were built. Then the two superposed turbulences were introduced into the nonlinear rigid body equations of motion to simulate the perturbation motion of receiver aircraft. The result shows that the superposition method can easily and effectively simulate the complicated wind disturbance. The study can provide reference for further research of the aerial refueling control system.