摘要
通过对箱式倾斜发射导弹在发射过程中的受力分析,建立了导弹在半约束运动状态下的发射扰动数学模型,通过Matlab/Simulink进行了数学仿真,仿真结果与实弹飞行测试结果一致,验证了所建立的初始扰动数学模型的正确性与实用性。
In this paper, the forces that act on the slant-launch missile during its launch course were analyzed. The model of launch disturbance of missile was established under a half-restriction state. The mathematical simulation was processed using the Matlab/ Simulink toolbox,the result of simulation was accordant with that of live round flight test. The correctness and the practicality of the mathematical model of initial disturbance were validated.
出处
《弹箭与制导学报》
CSCD
北大核心
2010年第5期76-78,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
