飛行自動控制 的英文怎麼說
中文拼音 [fēihángzìdòngkòngzhì]
飛行自動控制
英文
automatic flight control- 飛 : Ⅰ動詞1 (鳥、蟲等在空中活動) fly; flit 2 (利用動力機械在空中行動) fly 3 (在空中飄浮遊動) fly...
- 行 : 行Ⅰ名詞1 (行列) line; row 2 (排行) seniority among brothers and sisters:你行幾? 我行三。where...
- 自 : Ⅰ代詞(自己) self; oneself; one s own Ⅱ副詞(自然;當然) certainly; of course; naturally; willin...
- 控 : 動詞1 (告發;控告) accuse; charge 2 (控制) control; dominate 3 (使容器口兒朝下 讓裏面的液體慢...
- 制 : Ⅰ動詞1 (製造) make; manufacture 2 (擬訂; 規定) draw up; establish 3 (用強力約束; 限定; 管束...
- 飛行 : flight; flying; aviate; voyage; volitate; hop
- 自動 : 1 (自己主動) voluntarily; of one s own accord 2 (不憑借人為的力量) automatic; spontaneous 3 ...
- 控制 : control; dominate; regulate; govern; manage; check; cybernate; manipulate; encraty; rule; rein; c...
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Flying fish automatic industrial washing machinery series can wash, bleach dewater at medium or high speed, etc. the whole process is automatically controlled with micro computer, and some steps also can be operated manually
飛魚系列全自動工業洗衣機,即洗、脫兩用機,具有洗滌、漂洗、均布、中脫、高脫等功能,採用微電腦進行全過程的自動化控制,也可對各步驟進行手動操作。Whenever pearl saw anything to excite her ever active and wandering curiosity, she flew thitherward, and, as we might say, seized upon that man or thing as her own property, so far as she desired it ; but
珠兒只要看到有什麼激勵她的永遠活躍的好奇心,就會飛到那兒,只要她願意,我們可以說,她會把那個人或物當作自己的財產一般抓到手裡而絕不因此而稍稍控制一下自己的行動。This dissertation studies the problem of dynamics modeling, dynamical response, and distribution of moving mass for a re - entry vehicle ( mmcrv ) under the background of national natural science fund project “ precision control and guidance for moving mass control of a re - entry vehicle based on the virtual displacement concept ”
本論文以國家自然科學基金項目「基於虛位移概念的變質心再入飛行器精確制導問題研究」為背景,研究基於變質心控制的再入體動力學建模、動力學響應和落點分佈等問題。This design method overcomes the traditional autopilot ' s disadvantage that should shift the autopilot ' s gain according to flight phase ; it also can make the btt missile fly stably along the whole trajectory, and can intercept a maneuvering target accurately
該設計方法克服了傳統自動駕駛儀在控制導彈飛行中需逐段切換增益的不足,能控制btt導彈在大空域內沿全彈道穩定飛行,並能精確攔截機動目標。A integrated flight / propulsion control ( ifpc ) theoretical schema was designed based on this concept and a engineering schema was developed after take consideration of currently engineering condition and the requirements of in - service aircraft upgrade. a auto - flight system was designed which can achieve accurate flight movement control and increase performance of flight task such as ascend, cruise, te
基於該概念設計了飛推綜合原理方案,並在考慮工程實現條件及現役飛機改進、改型要求后建立了工程實現方案,設計了軌跡跟蹤方式的自動飛行系統,解決了軌跡生成、表示、管理、跟蹤等問題,能夠實現運動狀態的精確控制,提高爬升、巡航等任務的性能。Self - repairing flight control system ( srfcs ) is a kind of active - and passive failure tolerant control based on the fly - by - wire flight control system, and it is also an important tendency of the future flight control system
自修復飛行控制系統( srfcs : self - repairingflightcontrolsystem )是在電傳飛控系統基礎上發展起來的一種與主動容錯技術結合的先進飛控系統,也是未來戰斗機飛控系統的重要發展方向。After target is detected the on - board avionics suite in combination with the automatic control system of the helicopter solve the task of bringing the helicopter to the designated point and automatic firing of the weapons selected by the pilot
當捕獲目標后,機上的自動控制系統與電子系統將解算任務數據,引導直升機飛向敵潛艇水域,並在飛行員指令準許下自動發射武器進行攻擊。The control laws of longitudinal and lateral - directional autopilot modes are designed based on root locus theory. the control laws of altitude holding mode, heading holding mode, auto - throttle control and air speed holding mode are designed as well
研究了無人機的飛行控制技術,利用根軌跡法設計了無人機的縱向與側向姿態保持控制律,設計了高度保持、航向保持、自動油門及速度保持控制律。The oil loading system and the management of oil bin in the oil - bin area is intensive and the measurement method is under - developed at present time. in order to resolve this problem and realize the automatic management, this thesis analyzed the demands of the system, and then integrated the optical fiber sensing technology, the advanced computer technologies of hardware and software, the technologies of intelligent instrument, auto - control and communication ; finally a distributed and intelligent monitoring system of the automatic oil - loading system was developed. the thesis contains hardware design, software design and communication design
為了解決罐區裝車手動付油與油罐手工檢尺測量勞動強度大,方法落後以及油庫安全性要求非常高的問題,提高油庫自動化和信息化管理水平,本文從監控系統用戶需求與功能分析入手,結合當前飛速發展的光纖傳感技術、計算機軟體、硬體技術、智能儀表技術、自動控制技術和通訊技術,開發了一套用於石化行業的基於光纖傳感技術的集自動付油管理及儲油液位、溫度等安全檢測功能於一體的油罐庫區自動付油管理系統。On the basis of these, a simplified iced aerodynamics model is established, describes the effects of aircraft icing on aerodynamic parameters. main principle and implement method of iced aircraft envelope protection system are proposed. after ascertain iced aircraft envelope, for pilot and autopilot, open - loop and close - loop aircraft envelope protection control law respective designed, ensure the aircraft will efficiently follow the flight path specified by the pilot in the safe - flight envelope
在此基礎上,建立了簡化的飛機結冰氣動模型,以描述結冰對氣動參數的影響;給出了結冰飛行包線保護系統的基本原理及實現方法,在計算確定結冰飛行包線后,對於人工駕駛、自動駕駛飛行兩種情況,分別設計了開環、閉環飛行包線保護控制律,保證飛機在安全飛行包線內沿著預定的航線飛行。And the traditional designed autopilot has poor robustness, so it should shift the autopilot ' s gain for the btt missile flying stably along the whole trajectory
又由於用傳統方法設計的自動駕駛儀魯棒性不高,為控制導彈沿全彈道飛行,需逐段切換自動駕駛儀的增益。Target state estimater ( tse ) is an important and indispensable part of integrated flight and fire control system ( iffcs ). this article takes the ground mobile object as the study model. it established the system state equation and observation equation from the perspective of promoting system accuracy, simplifying the calculation and facilitating the engineering realization, the tse was set up by using the kalman filtering calculation method in the wake of linearizing the observation equation to make it adapt the precondition
目標狀態估計器是綜合飛行/火力控制系統中的一個重要組成環節,本文以地面機動目標為模型,從提高目標估計精度、簡化計算以及便於工程實現為出發點,建立目標的狀態方程及觀測方程,並對其進行線性化,利用自適應卡爾曼濾波演算法構造目標狀態估計器。Self - repairing flight control system ( srfcs ) is a kind of active and passive failure tolerant control based on the fly - by - ewire flight control system, and it is also an important tendency of the future flight control system
自修復飛行控制系統( srfcs : self - repairingflightcontrolsystem )是在電傳飛控系統基礎上發展起來的一種與主動容錯技術結合的先進飛控系統,也是未來戰斗機飛控系統的重要發展方向。Bus controller ( bc ) is an important component in fulfilling the automation of aviation electrical load control and management, whose primary task is to monitor and control the major bus of aircraft ' s electrical system
匯流條控制器是實現航空電氣負載控制與管理自動化的重要組成部分,其主要任務是對飛機電氣系統主匯流條進行監測與控制。Since it is a pig tyrants, and of course porcine link between. games, the player control of a vehicle carrying a porcine, escape from the bullets hit around. key control feizhu next move around, the game system is unique in the escape process, players can use insurance space bar is the instant removal of the bullets around to help their escape, xu li chutes to the left, with the game and xu li trough will slowly increase with a slow groove, increase a life, and the release of a p
方向鍵控制飛豬上下左右移動,游戲系統較為特殊,在躲避過程中,玩家可以使用「保險」空格鍵即瞬間清除周圍的子彈,幫助自己逃脫,左下方為蓄力槽,隨著游戲的進行,蓄力槽會慢慢增加,一條槽蓄慢的話,會增加一次生命,而玩家如果釋放一次「保險」則會扣去一條生命,注意,只是扣去一條生命,並不會減少已經積蓄的能量槽,但如果被子彈擊中的話,不僅失去一次生命,還會清空槽中已經積累的能量。Automatic flight control equipment
飛行自動控制裝置The automatic control system, as a critical technology, has an irreplaceable effect in keeping flight security and promoting attack efficiency. so high - qualified flight control system is necessary for completing the complex flight missions
飛行自動控制系統作為現代飛機的一項關鍵技術,在保持飛機飛行安全和提高攻擊效率方面起著不可替代的作用,所以高性能的武裝直升機的飛行控制系統的設計和使用是保證其完成復雜飛行任務的必要條件。With the development of simulation - technology and virtual reality, virtual prototype based on system simulation, flight dynamics, electronic technique, autocontrol theory and cad / cam has been more and more widely applied to the military rehearsal and the design and manufactural process of major weapon system
隨著模擬技術特別是虛擬現實技術的發展,以系統模擬、飛行動力學、電子技術、自動控制理論以及cad cam技術等為基礎的虛擬樣機技術在大型武器系統的研製以及軍事演習等方面的應用愈加的成熟起來。Finally, system is simulated, and the results can satisfy the requests value of the aircraft landing system and it represents a strong robustness of aircraft landing control system
然後設計了自動著陸控制系統控制律,並進行了模擬,模擬結果滿足飛機自動著陸各項指標要求,表明所設計的自動著陸控制系統具有較強的魯棒性。Systematic theory and experimental investigation are carried out on active vibration control of adaptive lamina based on smart materials and structures in the airplane engine applications
本文對應用於飛機發動機的基於壓電智能結構的自適應葉片振動主動控制技術進行了系統的理論分析和實驗研究。分享友人