flight-control computer 中文意思是什麼

flight-control computer 解釋
飛行控制計算機
  • flight : n 1 飛行，飛翔；（鷹對獵物的）追趕。2 （候鳥等的）遷徙；飛行的一群。3 （光陰）飛逝。4 （思想等的...
  • control : n 1 支配，管理，管制，統制，控制；監督。2 抑制（力）；壓制，節制，拘束；【農業】防治。3 檢查；核...
  • computer : n. 1. 計算者。2. （電子）計算機；計量器。-ism 電子計算機主義〈認為電子計算機萬能等〉。-erite, -nik 計算機專家；計算機工作者。
  1. Dissimilar redundant flight control computer system

    非相似余度飛控計算機
  2. When testing begins, the computer of the tested uav flight control system will be connected into the network as a slave. the master of the system will diagnose faults should there be any ; otherwise it will set flight parameters and load flight course data for the slave

    檢測時，無人機的飛控系統計算機作為從機連入網路，如果從機的飛控系統沒有故障，主機將為從機設置飛行參數和裝定航線數據；如果有故障，則主機為從機飛控系統診斷故障。
  3. The modern unmanned helicopter flight control system is generally composed of the flight control computer, the servo driving mechanism, the sensor, and the ground monitor control system etc. in this thesis the research to the helicopter flight characteristics was conducted at first, and its flight dynamic model was preliminary discussed, especially the mathematic model under hung - stop condition was formulated and the algorithm of the controller was designed in detail

    現代無人直升機飛行控制系統一般由飛行控制計算機、伺服驅動機構、傳感器、地面監測控制等分系統組成。本文首先對直升機的飛行特性進行了研究，並且對飛行動力數學模型做了初步探討，尤其對在懸停狀態下的數學模型做了較為詳盡的公式推導和控制器的演算法設計。
  4. The paper studies the project of improving the reliability of flight control computer by using the dual cpu hot - redundancy technology

    本文主要對利用雙機熱備份技術來提高飛控計算機可靠性這一方案進行了前期研究。
  5. The method can be used for many flight control computers easily. the dual cpu hot - redundancy technology became a method to improve the reliability of flight control computer

    該方法實施簡單，易移植和工程化，具有較好的通用性，為提高飛控計算機可靠性提供了一種途徑。
  6. Focusing on the advance research of the flight control computer system of some type of a high altitude, long endurance unmanned aerial vehicles, this paper analyzes and research its staicture in techniques of redundancy fault - tolerance

    本文針對某型號預研高空長航時無人機飛行控制計算機系統的可靠性要求，運用冗餘容錯技術對其進行了設計研究。
  7. We implement the dual cpu hot - redundancy technology into the common uav which used pc / 104 in our country. the reliability of flight control computer can be improved rapidly only if we increase a little hardware and software by the dual cpu hot - redundancy technology

    該技術在我國無人機普遍使用的pc 104體系結構作為平臺的飛控計算機上實施，只需增加少量的硬體資源和軟體模塊就可以大大提高飛控計算機的可靠性。
  8. Firstly discussing basic type of computer redundant structure and characteristic of the systems, the self - monitoring dual redundancy computer systems is brought forward as the design scheme for the required flight control computer system. the redundant structure is researched about reliability by using markor model and is carefully designed

    首先分析了計算機冗餘結構的基本類型以及本次設計的要求特點，選擇了自監控二冗餘飛行控制計算機系統的設計方案，運用馬爾科夫模型對此冗餘系統的可靠性進行了計算研究，並且對此冗餘結構進行了詳細地描述及設計。
  9. Focusing on the flight control computer system of some type of airplane, this paper first analyzes the advantage and disadvantage of the structures of many kinds of fault tolerant flight control computer systems and their ability in tolerating fault, followed by summarizing the key design technology. the dual similar redundancy fault tolerant computer system is brought forward as the design scheme for the required flight control computer. also brought forward is the particular system design

    本文以某型號飛機飛控計算機系統為研究對象，首先分析了各種類型容錯飛控計算機體系結構的優缺點及容錯能力，總結了容錯計算機系統設計的關鍵技術，然後提出了二模相似余度容錯飛控計算機系統設計方案，詳細設計了以motorola公司生產的先進powerpc740微處理器為核心處理器、以高性能的國際標準化通用vme總線為內總線的交叉通道通信容錯計算機系統。
  10. Most countries in the world attach importance to the use of long - time uav ( unmanned aerial vehicle ) in the military. the kernel question of long - time uav is how to improve the reliability of flight control computer. the research of how to improve the reliability of flight control computer has became more and more important today

    長航時無人機的重要性尤其在軍事上已經得到國內外的高度重視，其核心飛行控制計算機（以下簡稱「飛控計算機」 ）的可靠性問題變的日益突出，對其容錯研究成為當今的熱點。
  11. At fixed time intervals, the gts data are decoded by the hko main computer and quality control checks are applied. objective analyses are then carried out for data at various standard pressure levels to produce grid point values. charts showing flight level winds, temperatures and other information are made available at the airport meteorological office ( amo ) for the provision of flight documentation and airway winds

    天文臺的主電腦定時對接收到的資料進行譯碼及質量控制檢查，跟著對各個標準氣壓層面的資料進行客觀分析，計出各網格點的數值，從而製作各巡航高度的風、溫度及其他資料的天氣圖，讓機場氣象所用來編制飛行氣象文件和航道風。
  12. At fixed time intervals, the gts data are decoded by the hko main computer and quality control checks are applied. objective analyses are then carried out for data at various standard pressure levels to produce grid point values. charts showing flight level winds, temperatures and other information are made available at the airport meteorological office for the provision of flight documentation and airway winds

    天文臺的主電腦定時對接收到的資料進行譯碼及質量控制檢查，跟著對各個標準氣壓層面的資料進行客觀分析，計出各網格點的數值，從而製作各巡航高度的風溫度及其他資料的天氣圖，讓機場氣象所用來編制飛行氣象文件和航道風。
  13. Based on the prior knowledge of flight navigation control, a combined navigation system is achieved by integration of dgps, magnetometer and atmosphere data computer

    基於飛行導航控制的先驗知識，對dgps 、磁航向計、大氣數據計算機等飛行導航傳感器獲取的飛行狀態信息進行綜合處理，實現了組合導航控制。
  14. The lamv features redundant ， independent computer systems for flight management ， stability ， and control

    Lamv的特色是用獨立的咒余計算機系統分別進行飛行管理、穩定性調整和控制。
  15. Since the computer failure, russian flight controllers say they have had only partial communication with computers that control the space station ' s navigation and life support systems

    電腦出現問題后，俄羅斯航天飛行控制人員說，他們只能與控制國際空間站的導航以及維持生命的電腦取得部分聯系。
  16. In view of the development of computer technology, it is feasible to simulate a helicopter, flight environment and control system designing by computer

    從計算機技術的發展情況來看，利用計算機模擬一架直升機、飛行環境以及控制系統設計是完全可能的。
  17. Using aircraft ' s onboard computer thoroughly, the srfcs could enhance the flight control system ' s reliability, survivability, maintainability and lower life circle cost ( lcc ) while do not use more hardware

    它的基本思想是：在不增加硬體配置的條件下，充分利用機載計算機的計算功能，提高飛控系統的可靠性，生存性，維護性，降低壽命周期費用。
  18. Using aircraft ' s onboard computer thoroughly, the srfcs could enhance the flight control system ' s reliability, survivability, maintainability and lower life circle cost ( lcc ) while do not use more hardware. failure detection and isolation ( fdi ) is the key technique of srfcs

    它的基本思想是：在不增加硬體配置的條件下，充分利用機載計算機的計算功能，提高飛控系統的可靠性，生存性，維護性，降低壽命周期費用。
  19. With the develop of computer techniques, the digital autopilot system has replaced the analog system. the analog system has not been able to adapt the developmental desire of modem autopilot system function. the digital autopilot system, of which the computre is main part, has put up tremendous superiority in aspect of flight control system

    隨著計算機技術的發展，數字式飛行控制系統逐步代替了模擬式系統。模擬式系統已不能適應現代飛控系統功能發展的要求，而以計算機為主的數字式系統卻在飛行控制方面表現出其巨大的優越性。
  20. A design method of integrated flight / propulsion control ( ifpc ) optimization computer based on digital signal processor ( dsp ) and control area network ( can ) bus is presented

    本文提出基於dsp和can總線的飛推綜合控制優化計算機設計方案，並研製成功原理樣機。
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