CAJ | 학술논문

直升机飞行模拟器根据任务需求需要仿真自动过渡过程。研究了自动过渡过程特定，并建立了高度自动过渡、速度自动过渡数学模型。针对模拟器特点，设计了模拟器中自动过渡的仿真结构图。利用直升机六自由度非线性模型对自动过渡过程进行了仿真，结果表明该方法能够实现直升机模拟器中自动过渡仿真功能任务需求。
직승궤비행모의기근거임무수구수요방진자동과도과정。연구료자동과도과정특정，병건립료고도자동과도、속도자동과도수학모형。침대모의기특점，설계료모의기중자동과도적방진결구도。이용직승궤륙자유도비선성모형대자동과도과정진행료방진，결과표명해방법능구실현직승궤모의기중자동과도방진공능임무수구。
Helicopter simulator will simulate the automatic transition process according to the mission requirements. This thesis studies the specific automatic transition process and builds the mathematic model of automatic transition on height and speed. In allusion to the characteristic of simulator, this thesis also designs the simulation structure chart of automatic transition process in stimulator. Besides, it also utilizes the six-freedom degree and nonlinear model to stimulate the automatic transition process, finding that this method can realize the mission requirements for automatic transition process of helicopter simulator.