| 1. | Paremeters and symbols of guidedmissile flight dynamics
导弹飞行动力学参数符号 |
| 2. | The measuring method of low rotate speed of flying missile
导弹飞行低转速测量方法研究 |
| 3. | Flight reliability test method study of cannon launched guided projectile
炮射导弹飞行可靠性试验法研究 |
| 4. | Analyzing to a stand off missile ' s flight characteristics , the as missile trajectory simulation is completed
在分析了典型防区外导弹飞行特点的基础上，进行空地导弹弹道仿真。 |
| 5. | The camera features extremely long recording time to capture extended duration events , such as vehicle rollovers and missile flights
高速摄像仪具有特长的拍摄记录时间，可记录如车辆倾翻导弹飞行等不同事件。 |
| 6. | The result open out the feasibility of direct lateral force / aerodynamic control . the control style can raise the missile mobile ability in terminal trajectory
结果揭示了直接侧向力气动力复合控制的可行性，这种控制方式可以提升导弹飞行末端的机动能力。 |
| 7. | Missile rudders are executive bodies of missile flight control system , all kinds of attitude motion of missile are depended on the actuator driver fins of rudders
导弹舵机是导弹飞行控制系统的执行机构，导弹的各种姿态运动都是靠舵机带动舵面偏转来实现的。 |
| 8. | In this paper which was in the background of some model antitank missle , adopting maximum likelihood identification method estimated the aerodynamic parameters of the missle , with using flight datas
本文以某型反坦克导弹为背景，利用导弹飞行试验数据，应用最大似然递推算法估算了该导弹的气动力参数。 |
| 9. | In this paper , i studied currently database technology , analyzed missile flight simulation needs , designed and developed certain air to surface missile simulating database system software
本课题以半实物仿真中的飞行仿真为实例，在研究当前数据库技术成果的基础上，结合飞行仿真的实际需要，设计并开发了某型面对空导弹飞行仿真数据库系统的软件包。 |
| 10. | The implement process using this method is given , and combined with the representative parameters at the entire missile flight trajectory , the control effect is analyzed by simulation , and the simulation result has demonstrated the method is valid
给出了应用该方法的具体实现步骤，结合导弹飞行的全弹道典型特征点参数，通过仿真实验说明了设计方法的有效性。 |
