flight control surface 中文意思是什麼
flight control surface
解釋
飛機操縱面-
Additional trials on aeronautical telecommunication network ( atn ), surface movement guidance and control system ( smgcs ), electronic flight strips ( efs ), secondary surveillance radar mode s data link and very high frequency data link ( vdl ) are planned for this year
此外，有關航空通訊網路、地面活動引領管制系統、電子飛行紙條、 s模式的二次監察雷達數據鏈路和甚高頻數據鏈路的進一步試行運作，亦計劃在本年進行。 -
This is a flight during which the aeromodel is aerodynamically manoeuvred by control surface ( s ) in attitude, direction and altitude by the pilot on the ground using radio control
本類系指由地面的運動員通過無線電遙控模型改變飛行姿態、方向和高度的項目。 -
The flight ' s atmospheric dynamic characteristics is considered, the aircraft is modeled as a combination of objects. most compositions, such as scene system, flight system, flight ' s sound and control surface are all simulated
）等建模軟體建立了相應的三維表現模型；模擬了飛機的主要系統：飛行系統、視景系統、儀表系統和音響系統。 -
3 ) definition of input designer concept for flight control system ( fcs ). a input designer was successfully constructed which can provide a effect almost the same as directly control over aerodynamic control surface through the careful design of inputs of fcs. this input design concept is very important for in - service aircraft upgrade where change of the original pcs is not allowed
3 ）提出了飛控系統輸入設計概念，並成功地構建了飛控輸入設計器，能夠在不改變原飛控系統條件下有效地提高舵面控制能力，獲得接近直接舵面操縱的性能，對于現役飛機改進、改型中飛機運動自動控制系統的設計具有非常重要的意義。 -
Primary flight control surface
主飛行操縱面 -
Composite material repair for various structural parts of aircraft, such as radome, flight control surface, etc
雷達罩、操作舵面等飛機部件日常復合材料修理工作 -
Abstract : the control reconfigurable aircraft with multi - surfaces needs robust basic flight control system to support enough time for failure detection and isolation. when partial surface loses, it can keep the damaged aircraft stable. in this paper, multivariable output feedback digital control laws are designed for the control reconfigurable aircraft ( cra ). the method uses fast - sampling digital pi controllers to design digital flight control tracking system. this paper gives the way to design the controller and analyze its robustness characteristics. the simulation results indicate that the controller is very robust and the output responses are fully satisfactory
文摘:控制可重構飛機要求其基本飛行控制系統對舵面部分缺損故障具有強的魯棒特性，在故障發生后保證飛機的穩定性，提供足夠的時間進行故障的檢測和隔離，為控制系統重構提供條件.本文採用高速采樣pi控制器設計輸出反饋跟隨系統，給出了控制器的設計方法，並分析了它對于控制舵面部分缺損故障的魯棒特性.模擬結果表明，這種控制器具有好的魯棒特性 -
Based on the flight datum of a300, the mathematical models and the normal control law of uav are built. separating the traditional flight control surfaces into several independent portions, we can reduce the influence of the control surface each and add redundance to the systems at the meanwhile
採用將傳統操縱面分離成為各自獨立的操縱面的方法，提高了操縱面的綜合作用效果，因而使無人機具有了傳統飛機所沒有的操縱面控制冗餘。 -
As a class of nonlinear multivariable objects, which characteristics is difficult to identify, the wing - in - surface effect crafts need adopt more complicated control laws and integrated information - control systems to ensure the flight safety and control efficiency
作為一類非線性、多變量且很難辨識的受控對象，地效飛機應採用更加復雜的控制律和信息? ?控制綜合系統，以最大限度地保證低高度的飛行安全和操控效率。
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