| 1. | ( 2 ) the study of combined control methods of an intercepting missile in atmosphere 1
(二)大气层内复合控制问题1确定拦截弹模型。 |
| 2. | Neither would it prevent cruise missiles or bombers , whose flights are within the earth ' s atmosphere , from hitting their targets
它也不能阻止巡航导弹或轰炸机击中它们的目标，因为这些导弹或轰炸机都在大气层内飞行。 |
| 3. | The main works of this thesis are research of the direct lateral force ' s application , on the exoatmosphere kinetic - kill vehicle and on the inner - atmosphere airdefence missile
本文主要研究了直接侧向力技术在大气层外动能拦截器和大气层内防空导弹中的应用。 |
| 4. | This paper integrates direct lateral force control with aerodynamic control , taking the anti - aircraft missile which has the anti - guided ability in the aerosphere as research subject
本文的研究对象为大气层内具有反导能力的防空导弹。主要研究内容为把直接侧向力控制与气动力控制结合。 |
| 5. | Aimed to solve problem of airdefence missile end control invalidation , a new idea of building direct lateral force control in terminal trajectory is presented , and the optimal action position , mode and range are analyzed
(二)直接侧向力在大气层内防空导弹中的应用1 、针对防空导弹末端飞行失控问题，提出了建立末端直接侧向力控制的新思路。对直接侧向力最佳作用位置、最佳作用方式、最佳应用范围进行了分析。 |
| 6. | By analyzing the relation between the refractive index and the temperature and the stress field of the optical window in the aero - dynamic environment , according to the thermal - optical effect and the elasto - optical effect , we obtained the relationship of the index - of - refraction and temperature and stress , and explored the further study method of the aero - optical effect
摘要首先从热光效应和弹光效应的角度，分析了飞行器在大气层内飞行时，在气动热环境中的材料折射率与温度场和应力场的关系，得出了温度和应力对材料折射率的影响关系式，并进而探索气动光学效应下一步的研究方法。 |
| 7. | Lateral jet control technology is researched in this dissertation , based on supersonic / hypersonic missile aerodynamics and lateral jet interaction ( ji ) effects associated with the attitude control solid - propellant rocket motors system in the low endoatmospheric range
横向喷流干扰效应研究在超声速高超声速导弹总体设计和精确制导技术研究领域一直占有重要地位。本论文针对大气层内超声速高超声速导弹采用姿态固体火箭发动机侧喷流控制技术的一些问题进行了研究。 |
| 8. | 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。 |
| 9. | Of course , that doesn ' t mean that flying a battleship in the atmosphere of a planet will be safe either : you will have to be careful with your speed and the pressure of “ air ” on the hull , or the temperature ; you will have to carefully watch your fuel as the bottom thrusters will be continuously firing to maintain you in flight ; and if you disable the automatic compensation or have damaged thrusters , you might have to play “ lunar landing ” with your ship
当然，那并不说明在大气层内用战列舰也安全：你需要注意你的速度，以及空气对船身的压力，还有温度；当底部推进器持续的点火来维持飞行，你将要小心的注意你的燃料；如果你的推进器损坏，而且解除自动推力补偿系统，那么你只有玩“月球登陆”了。 |
