歼击机

jiān jī jī
  • fighter plane;fighter
歼击机歼击机
歼击机 [jiān jī jī]
  • [fighter] 用来歼灭敌机和其它空袭兵器的军用飞机

歼击机[jiān jī jī]
  1. 歼击机全动平尾转轴梁的可靠性分析

    Reliability analysis of the transmission shaft of the all-moving horizontal tail for a fighter plane

  2. 歼击机飞行员基本认知能力测验信效度分析

    The reliability and validity analysis of the basic cognitive capability test assessing the abilities of the fighter plane pilots

  3. 歼击机飞行员鼻窦冠状扫描CT影像分析

    CT corona scanning graph analysis on fighter aviator 's paranasal sinuses

  4. 580例歼击机飞行员的基础+Gz耐力检查结果分析

    Analysis of the relaxed + G_x tolerance records of 580 fighter pilots

  5. 迫切需要制定高G抗荷训练方案,以提高歼击机飞行员+Gz耐力。

    Fighter pilots should actively carry out anti G training in order to enhance their + Gz tolerance .

  6. 歼击机部队须增添G耐力训练特制设备,制定科学的体能训练计划。

    It is recommended that the special equipment of G-tolerance training should be added to the fighter aircraft units .

  7. 目的评价肌力协调抗荷训练对高性能战斗机飞行员和歼击机飞行员的抗G效果。

    Objective To evaluate the anti G effect of coordinated muscle straining training in high performance fighter pilots and Jian fighter pilots .

  8. 目的测量颈椎间孔的大小,探讨我国歼击机飞行员高G载荷对其颈椎组织可能产生的影响。

    Objective To measure size of cervical intervertebral foramen , explore the effect of high-G load experienced by fighter pilots on their cervical spine .

  9. 36例歼击机飞行员24h动态心电图分析

    An Analysis of Dynamic ECG of 36 Pilots

  10. 歼击机飞行员累加Coriolis加速度耐力试验调查

    An experimental study of cumulative Coriolis acceleration tolerance in fighter pilots

  11. 某型歼击机XX升机身副油箱尾锥振动故障分析研究

    The structural vibration breakdown analysis research on the Fighter-XX centerline drop tank 's tail cone

  12. 其次,利用T-S模糊模型对系统进行近似建模,应用基于模糊模型的模糊H∞跟踪控制律对歼击机进行输出跟踪控制。

    Second , the T-S fuzzy model is adopted for modeling of the known nonlinear system approximately , meanwhile fuzzy-model-based H ∞ tracking control law is designed to track the desired output signal .

  13. 目的调查歼击机飞行员累加Coriolis加速度耐力水平和运动病易感者脱敏习服训练效果。

    Objective To investigate the cumulative Coriolis acceleration tolerance in fighter pilots and the effect of desensitization and habituation training in the pilots susceptible to airsickness .

  14. 再次,应用基于T-S模糊模型和自适应神经网络的跟踪控制方案,对歼击机在各种故障条件下进行了自修复控制的仿真研究。

    Third , self-repairing control of some kind of fault states of fighter is studied by using the robust adaptive tracking control method based on the fuzzy T-S model .

  15. 本文最后依据计算机三维可视化技术、Visualc++面向对象的编程理论和OpenGL三维图形库,对歼击机进行了自修复控制的三维动画仿真研究。

    At last based on the technology of 3D_Visualization theory of the Object-Oriented of Visual C + + programming and OpenGL Graphic Library , a module of realization 3D graphics arithmetic is developed to the study of the self-repairing flight control system .

  16. 方法:对F5、F6和F7三代歼击机共230例飞行员的耳鼻咽喉病症谱进行对比分析。

    Method : It was analysed that disease spectrum of otorhinolaryngology in230 pilots of three generation fighter , named as F5 , F6 and F7 .

  17. 根据工效学实验的结果数据和飞行员的使用性评价意见,提出新型歼击机HUD数传指令显示的优化方案。

    According to the experimental results and pilots'ratings , the optimized display schemes of HUD ground-air data transferring commands in new fighters were advanced in this study .

  18. 考虑到工程的实际要求,本文还采用C++语言对第四代歼击机模型和动态逆控制律进行描述,并使用DLL动态链接库对软件进行了封装。

    Consider the engineering implement and the idiographic request of Air Force Equipment Department , we use C + + to describe dynamic inversion control law and model of the fourth generation fighter and encapsulated the software as a DLL .

  19. 方法采用宋华淼等编制的飞行人员心理健康量表(MHI),对来院疗养的342例强击、歼击机飞行员进行心理测评。

    Methods Pilots ' mental health inventory ( MHI ) compiled by Song was applied to the mental evaluation of 342 attack and fighter plane 's pilots admitted to the sanatorium .

  20. 通过对某型歼击机专家故障诊断知识的研究,研制了多媒体歼击机故障诊断专家系统MAFDES。

    Passing to fault diagnosis intellective study of aircraft expert , expert system of multimedia aircraft fault diagnosis ( MAFDES ) is built .

  21. 目的:研究以KH-x扩大囊覆盖面积抗荷服、无胸部代偿的抗荷加压呼吸及PHP动作组成的某型歼击机综合抗荷措施的抗荷效果;

    Aim : To observe the protection effect of a new combined anti-G measure which was composed of KH-x anti-G suit , unassisted PBG ( positive pressure breathing for G , PBG ) and PHP maneuver .

  22. 针对歼击机操纵面结构故障,提出了一种基于自适应不对称高斯基函数网络(AGBFN)的可靠跟踪控制方案。

    A reliable flight tracking control scheme is developed for a fighter in the presence of control surface failures based on adaptive asymmetric Gaussian basis function network ( AGBFN ) .

  23. 480例歼击机飞行员体检资料分析

    The analysis of the medical examination materials of 480 fighter pilots

  24. 新型歼击机应急操纵时的显示信息及其优先级

    Display information and its priority for emergency control of advanced fighter

  25. 60例正常歼击机飞行员颈椎间孔X线测量分析

    Analysis of radiographic of 60 normal fighter pilots cervical intervertebral foramen

  26. 歼击机飞行员屈光不正构成变化的研究

    Study on changes in the composition of fighter pilots ' ametropia

  27. 歼击机空战占位的模糊神经网络方法

    Fuzzy-Neural Network Method Used in Occupying Attack Position In Air Combat

  28. 护航歼击机的最优火力分配策略

    Optimal Fire Distribution Strategy of Escort Fighter Aircrafts in Air Combat

  29. 歼击机拦截巡航导弹效能的初步研究

    A Preliminary Study of Effectiveness of Fighter Aircraft Intercepting Cruise Missile

  30. 歼击机近距引导效能评估

    Evaluation on Efficiency of Short-Distance Navigation of Fighter Plane Guiding Skill