CAJ | 학술논문

为降低成本、提高准确度，仿真技术成为导弹飞行研究的重要方法。本文研究了导弹飞行轨迹及姿态的解算，对飞行导弹进行了力学分析与建模。在分析导弹飞行特点和姿态参数求解算法的基础上，动态模拟了垂直平面内弹体飞行轨迹，并实时显示了弹体的姿态。本文实现了实验室环境下对导弹飞行过程的描述，为导弹实际飞行研究提供了参考。
위강저성본、제고준학도，방진기술성위도탄비행연구적중요방법。본문연구료도탄비행궤적급자태적해산，대비행도탄진행료역학분석여건모。재분석도탄비행특점화자태삼수구해산법적기출상，동태모의료수직평면내탄체비행궤적，병실시현시료탄체적자태。본문실현료실험실배경하대도탄비행과정적묘술，위도탄실제비행연구제공료삼고。
Simulation has become an important method for missile flight research to reduce cost and improve accuracy .This paper concerns missile flight trajectory and attitude calculation .As a result ,mechanical analysis and modeling are done ,the characteristics of missile flight decoding algorithm and attitude parameters are analyzed ,the missile trajectory is dynamically simulated in a vertical plane and the missile attitude is real-time displayed .The description of missile flight process in a labo-ratory has provided a basis for actual missile flight .