摘要
为了研究某型反坦克导弹改进方案中气动外形选择以及推力(速度)方案、控制参数设计和敏感参数分析等方面的问题,在建立了相应数学模型的基础上,利用数字仿真方法,通过与原型导弹的飞行性能对比,提出了改进方案,进行了有关参数的设计与分析,对便携式反坦克导弹的改进有一定的参考价值。
In order to study the choice of aerodynamic configuration, the scheme of propulsive force(velocity),design of control parameter and sensitive parameter etc in the modified process of an antitank missile ,mathematical models are built ,and digital simulations are carried out. Modified scheme has been proposed by copmared with the flying properties of the archetype missile ,and corresponding parameters are designed and analyzed. It has guiding significance to the modified work of the portable antitank missile.
出处
《战术导弹技术》
1999年第1期54-58,64,共6页
Tactical Missile Technology
关键词
反坦克导弹
总体方案
弹道
数学模型
数字仿真
Antitank missile Modified scheme Aerodynamic configuration Control parameter Trajectory Mathematical model Digital simulation
