| 1. | Atbm advanced tactical ballistic missile
高级战术弹道导弹 |
| 2. | Anti - tactical ballistic missile
反战术弹道导弹 |
| 3. | Miss distance simulation for kinetic kill vehicle intercepting tactical ballistic missile
动能拦截器拦截战术弹道导弹的脱靶量仿真 |
| 4. | Computer simulation of damage efficiency for aircraft carrier under attacking of tactical ballistic missile
弹道导弹对航空母舰打击效果的计算机仿真 |
| 5. | Abstract : based on the actual combat results of the ballistic missile , this paper describes the measures of the tactical ballistic missile penetration and its equipments
文摘:在简述弹道导弹在战争中的实战效果的基础上,介绍了战术弹道导弹突防的措施与装备。 |
| 6. | Simulation models for the research of damage efficiency for aircraft carrier under the attacking of tactical ballistic missile were made , and the structure and function and algorithm were discussed
建立了用于研究弹道导弹对航空母舰打击效果的仿真模型，并讨论了模型的结构、功能和算法。 |
| 7. | The results show that the performance of the combined control system designed in this thesis was superior to the traditional only aerodynamic control system , and the warhead of tactical ballistic missile with medium velocity could be intercepted
结果表明，所设计的复合控制系统较纯气动力控制系统性能有所提高，能够拦截中等载入速的战术弹道导弹。 |
| 8. | From the point of view of attack - defense of tactical ballistic missile and aircraft carriers and through analyzing the mobile area and scouting early warnings and mobile evading capability of aircraft carrier the tactical ballistic missile ' s optimum attack tactics and aircraft carrier ' s defense tactics were made
摘要从常规弹道导弹与航空母舰攻防对抗的角度出发，通过对航母机动区城及侦察预警、机动规避能力的分析，确定了双方的最优攻防策略。 |
| 9. | 5 . aiming at the specific mission that intercept the warhead of tactical ballistic missile , the new issue for designing the guidance law is analyzed , and a new guidance method that fit for the mid - course is presented , based on the idea of predicting the intercept point . to design a feasible terminal guidance law , the shortcoming existing in the proportional navigation when intercepting the warhead is firstly
针对拦截战术弹道导弹这一特殊任务，分析了导引律设计面临的新问题，提出了以预测拦截命中点为思想的中制导段导引方法，研究了末制导段比例导引律弹道形状和过载分布特点，在此基础上为了改善比例导引律的缺陷，引入了目摘‘要标机动加速度和导弹轴向加速度等信息、 ，又寸比例导引律进行了修正，井对导引律中各参数进行了优化。 |
| 10. | The main works of this thesis are research of lateral force control and guidance of interceptors , emphasized on the terminal phase when intercepting the tactical ballistic missiles , including the performance analysis of extra - atmospheric kinetic - kill vehicle piloted by trajectory - control and attitude - control systems , and combined control of aerodynamics with lateral jets in atmosphere
本文主要研究拦截弹在拦截战术弹道导弹时，末段的制导和侧向力控制问题，包括大气层外动能拦截器在姿控与轨控发动机作用下的性能分析，和大气层内侧向力与气动力复合控制研究。 |
