| 1. | Fault tolerant design of sins gps dvl integrated navigation system
制导航弹半实物仿真系统误差分析与建模 |
| 2. | Influence of aerodynamic parameters on the trajectory characteristics of finless - aerial - bomb
气动参数对无安定器航弹弹道特性的影响 |
| 3. | Study of target acquisition probability for laser - guided bombs with proportional navigation guidance law
激光比例制导航弹对目标的捕获概率分析 |
| 4. | Application of coordinate transformations in the hardware - in - the - loop simulation of integrated navigation system
航弹捷联惯导系统半实物仿真试验研究 |
| 5. | The aerodynamic parameters of a kind of bomb are calculated and compared with the experiment values
计算了某航弹改造后的气动力，并与吹风值进行了比较。 |
| 6. | The result is among the best ones in our country . and it provides reliable gist for analyzing the dynamic parameter of rocket bomb
结果表明，测量的相对误差小于1 ，达到国内先进水平，为分析航弹动态参数，提供了可靠的依据。 |
| 7. | The main work discussed in this article is : ( 1 ) through the framework and data flow charts expatiated the total frame and layout of the bomb with scgs
本文主要完成了以下工作： 1通过硬件结构图和数据流图阐述了航弹系统的总体结构和规划2 |
| 8. | ( 2 ) relating the requirement of whole system , designed the experiment to check the execution mechanism of scgs - the characteristics of electrical step vane mechanism
结合全系统的要求，设计实验检查了航弹系统的执行机构? ?步进电动舵机的特性3 |
| 9. | The surface finite element solver brought forward by woodward is improved . according to the improved solver , the interfere between bomb and plane is researched . the aerodynamic parameters of the bomb , which under the wing are calculated
本文对伍德沃德提出的面元法加以改进，并应用改进后的面元法对航弹机弹干扰进行了研究。 |
| 10. | The aerodynamic parameters are calculated under dynamic condition . according to the position and the posture of the bomb , the parameters are calculated every short interval until it leaves the interfere area
本文采用了在动态条件下求解航弹气动力的方法，每隔很短的一个时间间隔就根据弹体的位置和姿态重新计算其气动力参数，直至航弹脱离机翼、机身的干扰区。 |
