慣性導航系統 的英文怎麼說
中文拼音 [guànxìngdǎohángxìtǒng]
慣性導航系統
英文
g -inertial navigation system- 慣 : Ⅰ動詞1 (習以為常 積久成性; 習慣) be used to; be in the habit of 2 (縱容; 放任) spoil; indulge...
- 性 : Ⅰ名詞1 (性格) nature; character; disposition 2 (性能; 性質) property; quality 3 (性別) sex ...
- 導 : 動詞1. (引導) lead; guide 2. (傳導) transmit; conduct 3. (開導) instruct; teach; give guidance to
- 航 : Ⅰ名詞(船) boat; shipⅡ動詞(航行) navigate (by water or air); sail
- 系 : 系動詞(打結; 扣) tie; fasten; do up; button up
- 統 : Ⅰ名詞1 (事物間連續的關系) interconnected system 2 (衣服等的筒狀部分) any tube shaped part of ...
- 慣性 : [力學] inertia; inertance; sluggishness; the force of inertia
- 系統 : 1. (按一定關系組成的同類事物) system 2. (有條理的;有系統的) systematic
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At ancient times, people were navigated by means of sun, fixed stars, etc., while currently the common navigation systems are astronomic navigation, inertial navigation and radio navigation
以前,人們主要利用太陽、星星等自然天體。現在人們利用的導航系統主要有:天文導航系統、慣性導航系統、無線電導航系統三大類。Cains carrier aircraft inertial navigation system
航空母艦飛機慣性導航系統Fos paper completes softwar design of the navigation system based on vxworks
本文完成了新一代基於實時操作系統的平臺式慣性導航系統的總體軟體設計。Data fusing algorithm in geomagnetic aided ins
地磁輔助慣性導航系統的數據融合演算法Fundamentally an inertial navigation system is a dead-reckoning system with a very significant characteristic which differentiates it from more conventional dead-reckoning equipment.
原則上慣性導航系統是一種航行推算系統,與一般的航行推算裝置不同,它具有極明顯的特點。Error analysis and simulation of ring laser gyro strapdown inertial navigation system
激光陀螺捷聯慣性導航系統誤差分析及模擬計算First this thesis discusses the development of the virtual instrument, and the method of developing the real time software ; then designs a interrupted virtual driver, deduces and programs the realtime arithmetic of wanderazimuth strapdown inertial navigation, develops strapdown inertial navigation realtime software based virtual instrument with object - oriented programming language. the software is able to display multi navigation parameter and is able to be added the extensible function
論文討論了虛擬儀器技術的發展與現狀,研究了windows98平臺下實時性軟體的設計方法,設計了基於硬體的中斷虛擬驅動程序,推導和編程實現了游移方位坐標系捷聯式慣性導航系統計算機實時導航演算法,利用面向對象的可視化開發語言開發出基於虛擬儀器的捷聯式慣性導航實時軟體。該軟體能夠顯示多個慣性導航參數,具有故障報警顯示功能,根據需要可以增加新的顯示功能。As the cumulate error, inertial navigation system ca n ' t provide perfect position and navigation for the autonomous underwater vehicles ( auv ) in unstructured, complex and instable ocean in a long time. the application of terrain - aided navigation techniques to the updating of an inertia navigation system has been investigated
慣性導航系統是實現水下導航的一種重要方法,但慣性導航存在累計誤差,為了修正慣性導航的累積誤差,提高導航精度,本文將飛機、導彈等所使用的地形輔助導航系統,應用到水下航行器上,成功地滿足了自主水下航行器的導航需求。Surely, the inertial navigation has high precision, but it is also costly. acoustic tracking location is not a good way for voyage a long distance
慣性導航系統精度高,但設備昂貴,水聲定位系統不適合機器人長航時的導航定位。Consequently, computational models of all subsystems are constructed, such as the strapdown inertial navigation system ( sins ), the control loop applied in self - control period, the guidance system by applying the technology of television ( tv ) guidance and the guidance law of proportion navigation, the autopilot by applying the technology of overload control in terminal control period, and so on
建立導彈各個子系統的計算模型,主要有捷聯慣性導航系統、彈體、導彈自控段的控制穩定迴路、採用電視制導和比例導引制導律的導引系統,以及採用過載控制的自動駕駛儀,然後在此基礎上建立導彈各系統模擬模型。The first half of this thesis has done some pilot works on the strapdown inertial navigation theory founded on dual quaternion
論文的前半部分在建立基於對偶四元數的捷聯慣性導航系統理論方面作了一些探索性工作。Gyroscope is indispensable in the control systems and inertial navigation systems on the carriers, such as the plane, the missile, the ship ect
陀螺儀是飛機、導彈、艦船等運載體及慣性導航系統不可缺少的重要元件。The flight control system contains gps & ins, which insured auto takeoff & landing, as well as the whole flight process
飛行控制系統採用gps全球定位系統和慣性導航系統,可自動完成從起飛到著陸的整個飛行過程。This paper is on study on data sampling and processing techno1ogy of gyroscope in sins. the project of torpedo sins was demonstrated and put forward at first
本論文圍繞著捷聯慣性導航系統中陀螺儀的數據採集及處理技術和姿態矩陣解算進行了研究。Based on this main idea, first the thesis discusses the mathematics model of gyro and accelemeter, the initial alignment of north - pointed strapdown inertial navigation system, the method of calculation navigation, the method of generating flight orbit data, the method of ins / gps integrated navigation in detail. then the thesis develops the system generating flight orbit data and the system of real - time simulating strapdown inertial navigation with vc + + 6. 0
論文以此為核心展開:首先詳細討論了陀螺和加速度計的數學模型、指北式捷聯慣性導航系統初始對準和導航解算的演算法、飛行軌跡數據生成演算法、 ins gps組合導航演算法;然後利用visualc + + 6 . 0開發出飛行軌跡數據生成系統、捷聯慣性導航實時模擬系統。This paper combines the wanderazimuth strapdown inertial navigation system with virtual instrument and designs a inertial navigation virtual instrument software
本論文以游移方位坐標系捷聯式慣性導航系統為對象,與虛擬儀器技術結合起來,設計了一個慣性導航虛擬儀器軟體。The algorithm of strapdown inertial navigation system is also discussed and then use the flight - track generator to give a simulation, since a closed loop feedback integrated navigation system is designed in this paper, and the output of the filter must feed back to the strapdown inertial navigation system, the analysis of the algorithm in strapdown inertial navigation system is important. the scheme to design the trajectory of gps and the simulation of gps constellation are then studied, the simulation of gps constellation is given from the calculation of vernal equinox base on the principle of celestial mechanics, this method of different from other methods given by other paper and is useful to the research of satellite navigation system. a new method to abstract noise modal in integrated navigation system is proved to be useful in practice, this method, which is given by use the principles of stochastic processes, statistics, time series analysis, and system identification, is suitable for the kalman filter in integrated navigation system
如航跡產生器的設計,該航跡產生器是研究組合導航問題的前提,從國外一些研究組合導航系統的文獻中可以看出,設計這樣一個航跡產生器是非常必要的,所以本文自行設計了這樣一個系統;還討論了捷聯慣性導航系統中捷聯解算的方法,並進行了模擬研究,由於在本文設計的閉環反饋式組合導航系統中,對捷聯慣導系統的平臺誤差進行閉環控制,需要將濾波器輸出的校正量反饋到捷聯解算內部,所以必須對捷聯解算進行深入的研究和分析,更何況捷聯解算問題本身也是導航界的一個熱門研究課題;另外,本文還介紹了gps軌道及其星座模擬的設計思想和方案,與以往gps軌道和星座模擬不同的是本文從天體力學中計算春分點開始,逐步進行gps軌道及其星座模擬,這樣的設計方法對從事衛星導航的研究工作是有價值的;還對組合導航中誤差建模方法進行了研究,綜合運用隨機過程、概率統計、時序分析及系統辯識等方面的理論提出了一套適合組合導航卡爾曼濾波的誤差建模方法,並運用實際研究工作中的測量數據對該方法進行了驗證。The inertial navigation system ( ins ) has a close relationship with the development of navigation, aviation and spaceflight. and the precision of ins is determined by the platform stabilization loop to a certain extent
航海、航空和航天事業的迅速發展離不開慣性導航系統,而其中的平臺穩定迴路是事關導航精度的重要部分。Abstract : based on the integrated inertial navigation system mainly consisting of inertial navigation system ( ins ) and electrostatically supported gyro monitor ( esgm ), mathematical and hardware - in - the - loop simulation in the course of the development of the integrated navigation system is discussed in this paper
文摘:本文以用慣性導航系統( ins )和靜電陀螺監控器( esgm )為中心的綜合慣性導航系統為背景,討論了綜合導航系統研製過程中的數學和半實物模擬技術。The mechanically dithered ring laser gyro ( mdrlg ) is playing a more and more important role in inertial strapdown systems in our country
採用機械抖動偏頻的激光陀螺在國內的捷聯慣性導航系統中正起到越來越重要的作用。分享友人