自控導彈 的英文怎麼說
中文拼音 [zìkòngdǎodàn]
自控導彈
英文
homing mi ile- 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...
- 導 : 動詞1. (引導) lead; guide 2. (傳導) transmit; conduct 3. (開導) instruct; teach; give guidance to
- 彈 : 彈名詞1. (彈子; 小球形的東西) ball; pellet 2. (內裝爆炸物, 具有破壞和殺傷能力的東西) bullet; bomb
- 自控 : automatic control; autocontrol; self-control; automatic regulation; self-steering
- 導彈 : guided missile
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Identical autopilots are used to control the pitch and yaw motions if the missile has two planes of symmetry.
如果導彈有兩個對稱面,則使用相同的自動駕駛儀控制俯仰和偏航運動。In order to design the autopilot for a rear controlled missile we must make a first estimate of the required aerodynamic derivatives.
為了設計尾部控制導彈的自動駕駛儀,我們必須首先估算一下所需要的氣動力導數。Orbiting satellites were better at spying on enemies than wayward reconnaissance drones, and rockets destroyed targets more reliably than temperamental flying bombs did
按軌道運動的衛星比難以駕馭且以監控為主的無人駕駛飛機更好地偵查敵情,而且相對於我行我素的自動導航導彈而言,用火箭來毀滅目標更具可靠性。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。Simulation model of c of submarine - launched anti - ship missile
潛射反艦導彈自控段建模與實現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。In the family of precisely guided weapons, tv - guided weapon system is one of the widely used precise guided weapons. tv - guided weapon system is based on image processing, automatic control and information science. it extracts the location information of missile image from tv image, and guides the missile to attack the target
電視制導武器系統是廣泛投入實戰應用的精確制導武器之一,它將圖像處理、自動控制、信息科學有機地結合起來,從電視圖像信號中提取導彈位置信息並導引導彈擊向目標。Considering that the state variables can be measured easily and the autopilot can be designed expediently, the btt missile ' s control model in which all trajectory states can be measured is presented in this thesis
並考慮到狀態變量的可測量性和自動駕駛儀設計的方便性,建立了全彈道可測量的btt導彈控制數學模型。To avoid high frequency oscillation in the course of autopilot design, damping coefficient value was treated as a constraint, the rise time was taken as objective, and the other performance criteria were taken as constraints, then the robustness design problem was solved by multi - objective optimization method
摘要在導彈控制系統設計過程中,考慮了自動駕駛儀的高頻振蕩問題,將其轉化為系統的一個約束條件,同時把上升時間轉化為目標函數,其他設計指標視為約束條件,採用有約束多目標優化的方法解決了系統魯棒性設計問題。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。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 error spreading and improving of auto - control terminal point of anti - ship missiles
反艦導彈自控終點誤差散布及其改進It is a crucial question to stabilize missiles under stronger interactions, which has been hardly studied before. in this dissertation many significant result are given from the research of several correlative dynamic and control topics. an exhaustive summarization is made for free flight motion of spinning missiles
導彈自旋飛行引起的運動耦合、控制耦合及其它效應容易導致彈體失穩,實現較強耦合作用下彈道導彈自旋飛行姿態穩定控制是亟待解決的問題。The characters of bank - to - turn control technology determine that the btt missile ' s mathematical model having kinematical coupling, aero dynamical coupling, inertial coupling and control coupling. so the widely used stt missile ' s autopilot, which is designed to be three - channel independent ca n ' t meet the btt missile ' s control need
Btt控制技術的控制特點決定了btt導彈的數學模型存在運動學耦合、氣動耦合、慣性耦合和控制耦合等多種耦合因素,因此目前側滑轉彎( stt )導彈廣泛採用的自動駕駛儀三通道獨立設計方法已不能滿足btt導彈控制系統的設計要求。This thesis applies the robust h control theory to designing a btt missile ' s autopilot
本文利用魯棒h _控制理論設計了高性能btt導彈自動駕駛儀。Mixed weights cgpc is constructed for constrained cgpc, which has advantage in simplicity and efficiency. performance of ballistic missile ’ s servo system is improved by approximate constrained arithmetic. the effect of side force on stability of spinning missiles is studied by routh criterion, which proved to be more universal than others ’ work
針對線性角運動模型,直接採用勞斯方法,與前人工作相比具有更好的通用性和精確性;藉此方法近似分析了側向力對自旋彈道導彈穩定性的影響;研究了內模控制在彈道導彈姿態穩定系統中的應用。By simulation of this autopilot on standard state point and special state points, this robust control system ' s high - speed response ability and good robust stability is validated. under this autopilot ' s control, the btt missile can fly stably along many trajectories in a large airspace. 3
通過對所設計的自動駕駛儀在標稱點和給定特徵點進行模擬試驗,驗證了所設計的魯棒控制系統能快速跟蹤指令信號,並具有較好的魯棒穩定性,能控制btt導彈在大空域內沿多條彈道穩定飛行。By the 3d simulation of the missile trajectory, the evaluation index, such as the kill probability, the hit precision can be obtained
建立了電視自動尋的制導導彈的完整模型,包括了傳感器模型、過載控制模型、自動駕駛儀及導引頭模型。Initially a surveillance drone, the predator was given a laser designator to enable it to guide precision - guided weapons from other aircraft, and then acquired its own weapons in the form of hellfire missiles
「掠奪者」最初的原型是一架用於監控的無人駕駛飛機,它裝備了一個激光指示器來讓它能指示其它飛機上精準度高的武器的定位,並接著啟用自己的武器? ? 「地獄火」導彈。According to request that military put forward, the target car that subject research should have such characteristics as remote control, high precision, good safeguarding, needing no track, etc, so as to achieve purpose of course require correctly when training to carry on cannon static to static, static to move, move to static, move to move etc. target car transfer speed require low inertia, high accuracy, high dependability, stupid and getting excellent and kind systematically ; wireless communication system expect much dependability, better anti - interference ability ; computer control system demand and try one ' s best to adopt advanced technology, components and parts source of goods reliable, high dependability, structure to be simple, have serial communication, digital display, systematic trouble examine and function of showing etc. the job of this thesis is divided into three major parts : the proposition and confirming of the electric power pulls, specification requirement and selecting type of equipment of communication system, sureness of the computer control system scheme
根據軍方提出的要求,本課題研製的遙控坦克靶車應具有遙控、精度高、維護性好、無軌道、自帶動力等特點,以達到訓練時進行火炮或導彈靜對靜、靜對動、動對靜、動對動設擊等課目的要求。靶車調速系統要求低慣性、高精度、高可靠性、魯棒性好;無線通訊系統要求高可靠性、抗干擾能力強;微機控制系統要求盡量採用先進技術、元器件貨源可靠、高可靠性、結構盡量簡單,具有串列通訊、數字顯示、系統故障自檢及顯示等功能。本文的工作分為三大部分:電力拖動方案的提出及確定、對通訊系統的技術要求及設備選型、微機控制系統方案的確定。分享友人