滾轉導彈 的英文怎麼說
中文拼音 [gǔnzhuǎndǎodàn]
滾轉導彈
英文
rolling missile-
The aerodynamic characteristics of a projectile with wrap around fins are studied systematically in this paper, as follows : 1. the lift coefficients 、 drag force coefficients 、 pitch moment coefficients 、 pitch damping moment derivatives and roll damping moment derivatives are obtained from engineering calculation through looking wrap around fins as flat fins of the same projection aera
本文對某卷弧尾翼彈氣動特性進行了系統研究，主要內容與結論為: 1 .將卷弧翼按照相同投影面積的平板翼進行工程估算，得到升力系數、阻力系數、俯仰力矩系數、俯仰阻尼導數、滾轉阻尼導數曲線。The flying stability of the unguided projectile with wrap around fins could be influenced by the self - induced rolling characteristics and the cross coupling effects of the waf badly. it is necessary to study further on this special aerodynamic problems
卷弧翼存在自誘導滾轉特性、較嚴重的交叉耦合效應等特殊氣動問題，對于無控的卷弧尾翼彈而言，這很大程度上影響飛行穩定性。And still signal being sheltered model and deflection separation model when the missile is controlled non - rolling are built, separation process are digitally simulated to check the stability during it
提出信號傳輸遮擋模型，建立受控無滾轉時的偏差分離模型，實現導彈分離過程數值模擬和穩定性分析。Proceeding with the support " s force condition is analysed in the static and revolve state, the stress distributions in the contact areas of support and roller are researched by way of hertz theory, the tow - dimensional elastic movement of the contact area is studied by contact mechanics, and the formula and curve of movement regulation are deduced
從回轉窯靜止與運轉時支承的受力情況分析著手，依據赫茲接觸理論對托輪與滾圈接觸區的壓力分佈進行了分析，並用接觸力學方法研究了接觸區的二維彈性滑動，推導出回轉窯軸向下滑計算公式，從而得出回轉窯軸向下滑特性曲線。After introduced its task and construct of the controller of the homing gliding missile, the longitudinal and lateral motion equations are provided. a continuous fuzzy - pid control system combined the advantages of fuzzy control and pid control is presented, and could be guaranteed the stability of the system using popov stability criterion. the results of simulation show that the fuzzy - pid control is able to provide a better relative stability and robustness, also have better dynamic and static characteristics than the pure pid control
將模糊控制和pid控制相結合，研究了一種基於模糊pid的連續控制器，利用波波夫穩定判據判定該控制器是漸進穩定的，並將其應用於制導滑翔彈俯仰角、偏航角、滾轉角穩定迴路中，設計模擬結果表明，該種連續控制器可使系統獲得很好的穩定性和魯棒性，動、靜態性能比單純pid控制都有較大提高。The motion model and dynamics model of the rolling missile was constructed, and the thrust performance of attitude control system were presented
建立了滾轉導彈運動學和動力學模型，以及姿控發動機的推力模型。Based on the average mathematical model, the transfer function of the rolling missile was deduced, and the stability conclusion was deduced and applied to the research object
從滾轉導彈的均態數學模型出發，推導了滾轉導彈的彈體傳遞函數。分析了滾轉導彈的穩定性條件。The thesis tracks the research about the intercept technology oversea. the rolling missile model with attitude - control - system is established by referring to the figuration dimension of pac - 3
本文跟蹤國外研究，以「愛國者? 3 」導彈外形尺寸為參考建立了具有姿態控制系統的滾轉導彈模型。2. considering the difference of the rolling missile and the non - rolling missile, the mechanism of rolling missile control force and the control theory of rolling missile was analyzed rigorously
考慮到滾轉導彈與非滾轉導彈的不同，本文仔細分析了滾轉導彈控制力的產生機理和滾轉導彈的控制原理。分享友人