angular rate造句
例句與造句
- Sensor , piezoelectric , angular rate general specification for
壓電角速率傳感器總規(guī)范 - Barb british angular rate bombsight
英國角速度轟炸瞄準(zhǔn)器 - When there is an angular rate input , the fluid will deflect by the effect of coriolis acceleration
當(dāng)有角速度輸入時，射流束在哥氏力的作用下發(fā)生偏轉(zhuǎn)，偏轉(zhuǎn)的大小和方向取決于輸入角速度。 - A piezoelectric fluidic angular rate sensor ( pears ) is a kind of flow sensor . in this thesis peats were researched
Cjsys - a5型壓電射流角速度傳感器（以下簡稱壓電射流角速度傳感器）屬于氣流式傳感器，本學(xué)位論文對壓電射流角速度傳感器進行了研究。 - Calibration results indicate that this angular rate gyro has good linearity with correlation coefficient of 0 . 9996 , and high precision with standard error of 0 . 0036
標(biāo)定結(jié)果表明，該角速率陀螺線性度好，相關(guān)系數(shù)為0 . 9996 ；精度高，標(biāo)準(zhǔn)誤差為0 . 0036 。 - It's difficult to find angular rate in a sentence. 用angular rate造句挺難的
- Neural network has the ability of approaching nonlinear function at random precision , so that correct non - linear errors of angular rate sensor on the basis of neural network method
神經(jīng)網(wǎng)絡(luò)具有理論上以任意精度逼近非線性函數(shù)的能力，故本文采用基于神經(jīng)網(wǎng)絡(luò)方法來校正角速度傳感器的非線性誤差。 - Both results show that the inertial coupling of the platform to infrared camera scanning mirror , to evaluate mirror motion , is negligible and so the mirror can perform scans of the earth at the specified angular rate
兩方面的仿真分析表明:星體姿態(tài)運動干擾力矩對紅外相機掃描鏡轉(zhuǎn)動影響很小,紅外相機掃描鏡能夠按設(shè)計轉(zhuǎn)速正常運行。 - This paper developed a micro angular rate gyro based on micro piezoelectric ceramic rod structure instead of the sensitive double - deck structure as well as piezoelectric ceramic strain foils , and designed a phase - sensitive detection circuit
摘要研制了基于微型壓電陶瓷棒結(jié)構(gòu)代替雙敏感梁結(jié)構(gòu)及壓電陶瓷片的微型角速率陀螺，并設(shè)計了相敏檢波電路。 - Based on the mathematical model developed by the paper , the trim calculations are carried out in the conditions that the example aircraft converts from helicopter to airplane mode in level flight with zero longitudinal acceleration and angular rate
本文依據(jù)所建立的樣例機縱向動力學(xué)模型,假定飛機在給定高度平飛,縱向加速度和角加速度均為零,完成過渡模式下的動力學(xué)配平。 - Trough the analysis of the output of the detecting circuit of the capacitances , the processing circuit is designed , and the angular rate is separated : parameters computed of the gyroscope and the performance analyzed of the circuit show that the circuit can reach the base requirement
經(jīng)過對電路性能的分析、陀螺主要參數(shù)的估算，確定所設(shè)計的電一幾}北邢業(yè)人學(xué)學(xué)位論義路可以達至fj基本要求。 - The aerodynamics subsystem is designed employing classical control methodology , including the inner loop which adopt angular rate feedback to stabilizing the attitude , and the outer loop which track the guidance command , and the proper emendation nets are designed for each loop
采用古典控制理論來設(shè)計氣動力控制系統(tǒng)，包括具有角速度反饋的穩(wěn)定內(nèi)回路、跟蹤制導(dǎo)指令的外回路以及各校正環(huán)節(jié)的設(shè)計。 - Introduce the traditional two samples rotation vector algorithm and three samples rotation vector algorithm , which fit the incremental angular condition . but , the output of fiber optic gyro is angular rate of the vehicle , the error would increase serious if use traditional algorithm
由于光纖陀螺儀輸出為角速率信號,而傳統(tǒng)的旋轉(zhuǎn)矢量算法輸出為角增量信號,采用角增量提取算法,旋轉(zhuǎn)矢量精度會大幅大降。 - This setting could increase the damping of angular rates and improve the stability . based on bell stabilizer bar , bell - hiller stabilizer bar adds small wing on the two ends of bar . compared with main blades the aerodynamic forces and moments generated by the bar could be neglected
希勒伺服旋翼在貝爾穩(wěn)定桿的基礎(chǔ)上,于兩個質(zhì)量塊處添加了小翼,與貝爾穩(wěn)定桿相比,希勒伺服旋翼自身的揮舞運動借助機械耦合引起旋翼二次變距,起到改善操縱性的作用。 - To solve the problems caused by the varieties of the missile dynamics with the difference of flight height , velocity and attitude angle in modeling the missile , in this thesis , the theory of variable structure model reference adaptive control is used to design a pitch channel autopilot based on a longitudinal missile model , the status equation using the measurable parameters of load and angular rate is established , and the methodology to choosing the reference model is discussed also , and the performance of the controller is analyzed by means of simulation
為了解決攔截彈氣動參數(shù)隨飛行高度、速度、姿態(tài)的不同，變化范圍大，控制系統(tǒng)難以準(zhǔn)確建模的困難，基于縱向平面攔截彈模型，采用模型參考變結(jié)構(gòu)控制理論設(shè)計了俯仰通道姿控復(fù)合控制系統(tǒng)，以可測量變量過載和角速度作為狀態(tài)量建立了系統(tǒng)的狀態(tài)方程，討論了參考模型的選擇方法，并對系統(tǒng)的性能作了仿真分析。 - Here , the aircraft is in extreme flight conditions that is high angles of attack and high angular rates . it can encounter severe nonlinear effects . detailed descriptions of the flight dynamic , aerodynamic models , inverse dynamic and the choice of the control variable are given
2 、應(yīng)用經(jīng)典的微分幾何方法研究了一般的飛行狀態(tài)下飛機飛行的控制律，指出不利用矢量推力的飛行系統(tǒng)的控制方程一般都是可以逐步通過動態(tài)狀態(tài)反饋，適當(dāng)?shù)淖鴺?biāo)變換和正則靜態(tài)反饋等三個步驟得以線性化。
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