flying control system 中文意思是什麼
flying control system
解釋
飛機操縱系統-
Offers waterway and wetland maintenance, weed and algae control, fish stocking, stormwater drainage system services, flying insect control, wetland plantings, water testing, fountain installation and repairs
-集污水處理產品設計開發，設備，工程承包於一體。自主開發有懸掛鏈曝氣裝置及自動化控制系統，供應曝氣設備。 -
We also provide engineering services to the civil aviation department, supporting its air traffic control, radar and aviation control facilities located both within the airport and at other external sites. maintenance and operations support for government departments and the security forces include the police s trunk mobile radio handsets, fire services department s fire training simulator as well as the specialised e & m system at the government flying service s headquarters
我們亦為民航署位於機場內外的航空交通控制、雷達及航空控制設施等提供工程服務。此外，我們亦為紀律部隊等政府部門提供機電維修及操作支援服務，包括維修警隊的集束流動無線電手機及政府飛行服務隊總部的專門機電系統。 -
To ensure the precision of distance measuring, the high - speed laser driving circuit and the detect - amplifying circuit constituted by two class high - speed operational amplifiers are used in auto adaptive cruise - control system, and the laser flying time is measured by a sixteen bit ' s binary counter, whose counting frequency is 100 megahertz
為保障測距精度，裝置採用高速激光器驅動電路和由兩級高速運算放大器構成的探測放大電路，並用一個計數脈沖頻率為100mhz的16位二進制計數器完成激光收發間隔時間的測量。 -
It was analyzed about the problems of space vehicle flight control, the development of space vehicles, the design aim and main characteristic of flight control systems of varied space vehicles, the main design requirement of flight control system of reusable space vehicles, the key technology which have to be resolved in flying control law design and flight control system design
摘要分析了空間飛行器飛行控制系統要解決的問題，空間飛行器的發展過程，各類空間飛行器飛行控制系統設計目的和主要特點，可重復使用的發射飛行器飛控系統的主要設計要求，在設計要求的確定，飛行控制律設計和飛行控制系統設計中要解決的關鍵技術。 -
The ml converter is a multi - input and multi - output, strongly coupled nonlinearly system, its control elements ( duty cycles ) and the controlled elements ( output voltage and flying capacitor voltages ) of the ml converter are strongly coupled, so the system should be decoupled to multiple single - input and single - output sub - systems such that each output can be controlled independently
多電平變換器的控制量（各開關管占空比）和被控量（輸出電壓及各飛跨電容電壓）之間存在耦合關系，它是一個多輸入多輸出、強耦合的非線性系統，因此需要將其解耦成多個單輸入單輸出系統，以對被控量進行獨立的閉環控制。 -
Three axis optical tracking test table is a kind of powerful instrument used to reproduce the flying posture of flying weapons in laboratory. the test table, together with equipment producing target, simulates the attacked target and flying missile, which can really simulate the various flying postures in space and dynamic characteristics. thus, the performance of sensors, control system and actuator and so on can be tested and evaluated, which provides various reference bases for developing, improving and redesigning flying weapons
三軸光學跟蹤試驗轉臺是一種在實驗室條件下復現飛行器或導彈在空中飛行姿態半實物模擬的有力工具，它和目標發生裝置組合在一起模擬導彈跟蹤目標的過程，可以真實地模擬出導彈等飛行器在空間的各種姿態和動力學特性，從而對其傳感器件、控制系統和執行機構等硬體設備的性能加以測試和評價，為飛行器的研製、改進和再設計提供各種參考依據。 -
In this paper, dynamic inversion control law is designed to eliminate its global non - linearization and unstable aerodynamic force etc. and based on the time - scale separation principle, the control system can be divided into fast loop and slow loop. but there are still lots of unknown disturbances that may cause great damages to stability when flying
由於在飛行過程中大范圍非線性、具有非定常氣動力等特性，本文採用了非線性動態逆控制律來構成全局線性化的性質，根據時標分離的原則，設計了空天無人飛行器的快迴路和慢迴路控制器。 -
This dissertation takes system demonstration and validation of small satellites formation flying as the background, the theory and algorithms of relative attitude determination based on the gps like sensors are investigated ; the relative attitude coordinated control law, multi - agent based formation flying architecture and the coordination strategy are designed
本文以「微小衛星編隊飛行演示驗證方案論證」為研究背景，深入研究了基於類gps相對測量的星間相對姿態確定方案和演算法，設計了編隊飛行衛星multi - agent體系結構與協同工作流程和策略及相對姿態協同控制演算法。 -
Because the internal structure of high - speed long - range flying objects ( hslrfo ) is so complicated and the mass distribution is extremely non - uniform, the precision of the mass characteristic parameters obtained from theoretical calculation is not enough to be applied to the practical measurement and control. the special test system for the mass characteristic parameters of high - speed long - range flying objects, therefore, is in great need and it is also necessary to study its performance
由於高速遠程飛行物體的內部結構非常復雜，質量分佈不均勻，在科學研究過程中進行的理論計算得到的質量特性參數與其使用要求相差甚遠，基本不能作為計算和測控參數使用，因此必須研製專用的測量系統，並對測量系統的測量特性進行研究。 -
Based on the analysis of lateral - directional control system of a certain plane, representative fault infecting flying security is specialized ; flying security is evaluated ; it is found that flying security probability can not be content with the flying safety standard
摘要在對某型飛機橫向操縱系統分析基礎上，列舉出危害飛行安全的典型故障；針對該典型故障，進行了飛行安全評估；計算發現，飛行安全風險概率達不到安全標準。 -
The control system can monitor the flying simulation process real - time and change the flying environment parameters in correct time
通過控制臺系統可實時監控飛行模擬全過程，適時改變飛行環境參數。
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