CAJ | 학술논문

为简化指控系统解算流程，缩短指控系统解算尾流自导鱼雷带角射击参数时间，为后续的鱼雷模拟器的软件研制提供实现手段，提出在尾流自导鱼雷有利提前角射击弹道的基础上进行二次转角航行的改进的尾流自导鱼雷带角射击模型。依据尾流自导鱼雷射击原理，结合有利提前角射击和二次转角射击，对所提出的模型及其约束条件进行了分析与推导，简化了鱼雷带角射击参数的解算。深入分析了尾流自导鱼雷带角射击逻辑，提出采用面向过程设计方法对模型进行仿真，经过对仿真输出图形和仿真数据的分析，验证了所提出模型的准确性。
위간화지공계통해산류정，축단지공계통해산미류자도어뢰대각사격삼수시간，위후속적어뢰모의기적연건연제제공실현수단，제출재미류자도어뢰유리제전각사격탄도적기출상진행이차전각항행적개진적미류자도어뢰대각사격모형。의거미류자도어뢰사격원리，결합유리제전각사격화이차전각사격，대소제출적모형급기약속조건진행료분석여추도，간화료어뢰대각사격삼수적해산。심입분석료미류자도어뢰대각사격라집，제출채용면향과정설계방법대모형진행방진，경과대방진수출도형화방진수거적분석，험증료소제출모형적준학성。
In order to simplify the calculation process of command and control system and shorten the calculation time of launching parameters for launched with preset angles, a new trajectory model that the wake homing torpedo rotates twice on the basis of the trajectory launched with advanced angle is established. Depending on the launch principles of wake homing torpedo, the new mathematical model is established with analysis of the model and its constraint conditions. Furthermore, the logic of wake homing torpedo launched with preset angles is discussed, and the simulation of the logic model using the proce?dure oriented programming method is conducted. The analysis of the graphics and data from the simulation demonstrates the accuracy of the model.