attitude control technology 中文意思是什麼

attitude control technology 解釋
姿態控制技術
  • attitude : n. 1. 姿勢，身段。2. 態度，看法。3. 【軍事】飛行姿態。4. 芭蕾舞的一個姿勢。
  • 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...
  • technology : n. 1. 技術，工程，工藝。2. 製造學，工藝學。3. 術語（匯編）。
  1. Based on the spaceflight technology innovation program of “ research on the testing method of reliability - - - - research on the fault diagnostic expert system and neural network ” and the pre - research defense projects of “ research on longevous service and high reliability of satellites ” of the national tenth - five - year plan, taking attitude control system of a satellite as object, the theories and the applications of the neural networks and expert system in the fault diagnosis are studied in this dissertation

    本文以航天技術創新基金項目「可靠性試驗方法研究? ?故障診斷的專家系統神經網路技術研究」和國家武器裝備「十五」預研項目「衛星長壽命高可靠性技術」為背景，以衛星姿態控制系統為研究對象，在理論和實踐兩個方面對神經網路和專家系統相結合的故障診斷技術及其在衛星中的應用進行了研究。
  2. Space technology is the most influencing technology of moden science and technology. with widespread use of application satellite, people pay more and more attention to high accuracy and durability attitude control system

    航天技術是現代科學技術中最具有影響力的高技術之一，隨著通信、遙感等衛星的廣泛應用，高精度、長壽命的衛星姿態控制系統成為人們對衛星關注和研究的焦點。
  3. This thesis, taking geosynchronous satellite as an example, studies systematically and thoroughly the multi - sensor information fusion technology, studies fault diagnosis and system rebuild technology in satellite attitude control system, and studies autonomous navigation, orbital keeping technology

    本文以地球同步軌道衛星為研究對象，從理論上和工程上較系統和全面地研究了衛星姿態控制系統的多敏感器信息融合技術、故障診斷與系統重構技術、自主導航技術、軌道保持技術。
  4. For deep space explorer, the attitude control system design methods were studied in this dissertation, which is funded by the national 863 plan ( 2004aa735080 ), “ autonomy technology and simulation demonstration system for deep exploration ”

    本文結合國家863科研計劃項目「深空探測自主技術與模擬演示系統」 （ 2004aa735080 ） ，對深空探測器姿態控制系統設計方法進行了研究。
  5. Primarily, many persons still hold to hesitating attitude to network education, but along with various modern educational technology coming, the quantity of networked courses develop with times completely, the network education and elementary educations control complement each other, be in conjunction with the development

    在初期，不少人對網路教育還持觀望態度，但隨著多種現代教育技術的面世，完全可以使網路課程的質量與時俱進，網路教育與普通教育駕馭相輔相成，協同發展。
  6. At present, the most effective method of destroying the warhead of btm is the technology of directly hit kinetic kill, which can achieve precision control to the missile by adding the trajectory - control jet or attitude - control jet

    目前對付來襲tbm彈頭最有效的手段就是採用直接碰撞動能殺傷技術。它是通過在導彈上安裝響應快速的雙組元軌、姿控發動機以實現對導彈的精確控制。
  7. Algorithm research of the early - warning satellite attitude control under the payload disturbance is a critical technology of ballistic missile early - warning system

    預警衛星在其有效載荷干擾作用下的姿態控制演算法研究是彈道導彈預警系統的一項關鍵技術。
  8. The dynamic thrust measure technology for high - altitude simulation test of the attitude control liquid rocket engine was studied in the thesis

    本文研究的是姿控發動機高空模擬試車中的動態推力測試技術問題。
  9. At present, fes technology has been successfully applied in many fields such as uninterruptable power supply ( ups ) systems, electric power systems, hybrid electric vehicles, etc. researches indicate that in energy sources and attitude control system of satellites, by fess both energy storage and attitude control can be accomplished. it would be remarkable to improve global performance of satellites, so aeronautics & astronautics departments attach great importance to fess

    研究表明，在衛星能源和姿態控制系統中，利用飛輪儲能系統可以同時完成能量儲存和姿態控制兩方面的功能，這對于提高衛星的總體性能有著顯著的意義，因而得到航空航天部門的重視，並成為該研究方向的前沿課題，但目前尚未進入實用階段。
  10. Lateral jet control technology is researched in this dissertation, based on supersonic / hypersonic missile aerodynamics and lateral jet interaction ( ji ) effects associated with the attitude control solid - propellant rocket motors system in the low endoatmospheric range

    橫向噴流干擾效應研究在超聲速高超聲速導彈總體設計和精確制導技術研究領域一直佔有重要地位。本論文針對大氣層內超聲速高超聲速導彈採用姿態固體火箭發動機側噴流控制技術的一些問題進行了研究。
  11. In order to provide a basic and effective practical engineering tool for handling quality planning, analysing and evaluating, which is needed hi helicopter prototype development, this research work is launched on the fundation of comprehending the new aeronautical standard of united states army - ads - 33, and has obtained the achievements as following : ( 1 ) performance definition of pcs according to the criteria requirements for an explicit helicopter, beginning at analysis of its missions. ( 2 ) establishment of a helicopter attitude controller, which can meet the criteria requirements, by using the technology of adaptive neural network model - inverse control ; implementation of two response types ( rts ) and two control modes ; evaluation of quantitative parameters according to the ads - 33. ( 3 ) establishment of a helicopter trajectory contoller based on the attitude controller ; simulations of mission task elements ( mtes ) and evaluation of handling quality

    為了給型號研製中飛行品質的規劃、分析和評價提供基本的、有效的工程實用工具，本課題在充分消化理解美軍新航標ads - 33的基礎上，作了以下工作： （ 1 ）針對具體直升機，從任務分析入手，根據規范要求確定對飛控系統的要求； （ 2 ）應用自適應神經網路模型逆控制技術，構造了能夠滿足飛行品質要求的直升機姿態控制器，實現了兩種響應型式、兩種控制模式，並根據ads - 33進行了定量指標評估； （ 3 ）在姿態控制器的基礎上，構造了軌跡跟蹤器，進行了任務科目基元模擬和飛行品質評估。
  12. 4. conclude and verify detailedly attitude algorithm and conical scan control algorithm in process of initial alignment. on the base of static initial alignment technology, reach the dynamic initial alignment technology used on moving carrier

    四、對在初始對準中採用的姿態解算和圓錐掃描控制演算法進行了詳細的理論推導和模擬驗證，然後在靜態初始對準的基礎上，引出了用於載體移動過程中的動態初始對準。
  13. Now studying satellite attitude control subsystem with high precision and high. stability is the key technology of modern small satellite, which has received increased domestic and overseas attention, and it is also the promise and basis on which all kinds of space exploration, space exploitation and other space missions can be realized

    高精度高穩定度的衛星姿態控制系統作為現代小衛星的關鍵技術，業已受到國內外的廣泛關注，它也是實現衛星所擔負的各種探測、開發和空間任務的重要保證。
  14. In addition, the research has also yielded some obvious affecting factors, such as, small business owners who enjoy a high value of the technology, and an optimistic attitude to the profit, the level and structure of the work force in relation to the major means of accumulations, level and structure of the work force in relation to the developmental adaptability, quality control and standardization of the management in the process of the new product development

    影響公司構建其核心技術能力的關鍵問題有：技術企業家及主要研發者的技術價值觀和利益偏好；公司人力資本結構水平及其積累的主導方式；技術企業家人力資本結構與公司發展階段的適配程度；對新產品開發過程的質量控制和公司管理的規范化程度等。
  15. With the continuous development of the satellite technology and increase of the system complication, the design of software architecture for the attitude and orbit control system of satellite has become an important problem

    隨著衛星技術的不斷發展和系統復雜性的不斷提高，姿軌控系統軟體體系結構的設計成為衛星姿軌控系統一個重要的研究課題。
  16. Based on the requirements of high precision pointing / targeting of advanced spacecraft, dynamic modeling of spacecraft with flexible appendages bonded with piezoelectric sensors / actuators, attitude control and active vibration suppression theory are studied deeply in this dissertation, which is funded by the research fund for the doctoral program of higher education of china item ? “ large flexible multi - bodies structure spacecraft active vibration control technology ” ( 20050213010 ). the main contents of this dissertation are as the follows : an approximate analytical dynamic model of a flexible spacecraft with surface bonded piezoelectric sensors and actuators is derived using hamilton ’ s principle with discretization by the assumed mode method. the model is then converted to state - space form for the purpose of control design

    本學位論文結合高等學校博士學科點專項科研基金「撓性多體結構衛星主動振動控制技術研究」 （ 20050213010 ）課題，從理論上對粘貼有壓電智能元件的撓性航天器的建模、姿態控制和主動振動控制理論等展開了深入的研究，其研究內容主要包括以下幾個方面:利用hamilton原理推導了撓性航天器的動力學模型、壓電元件的作動方程及檢測方程，並採用模態分析方法，進一步將撓性航天器的耦合方程規范化，使之適應于姿態控制系統的分析和設計。
  17. The thesis tracks the research about the intercept technology oversea. the rolling missile model with attitude - control - system is established by referring to the figuration dimension of pac - 3

    本文跟蹤國外研究，以「愛國者? 3 」導彈外形尺寸為參考建立了具有姿態控制系統的滾轉導彈模型。
  18. The research on fault diagnosis and system rebuild technology in satellite attitude control system : the intelligent and independent algorithms about fault diagnosis and system rebuild technology in satellite attitude control system are put forward

    衛星控制系統故障診斷與系統重構技術研究：提出了基於聯邦濾波結構的衛星姿態確定系統智能自主故障診斷與系統重構方案和演算法。
  19. In this article, the following technology of the carbon fiber composite flywheel in the integrated energy - storage / attitude - control system are analyzed and the valuable achievements are achieved above the foundation of consulting a large quantity of literatures and investigation : 1. different technology method for carbon fiber composite flywheel are designed, aimed at the character of carbon fiber composite material and manufacture 2analyzes the stress of carbon fiber composite flywheels made by different technology method, hoop - winding method, symmetric ortho layers pressing method, multi - layer winding method and interference joining method, under high rotate speed, builds their static model ; and simulates their technology and shape parameter ' s affecting their stress level with i - deas f. e. m

    本文在查閱了大量國內外相關文獻及調研的基礎上，針對集成化儲能/姿態控制飛輪系統中的碳纖維復合飛輪的以下相關技術進行了研究，並取得了有價值的成果： 1針對碳纖維復合材料的特點及加工方式，設計了周向纏繞成型法、對稱正交鋪層層壓法、多層結構纏繞及過盈連接法等不同工藝方式的碳纖維復合飛輪轉子； 2針對不同工藝方式的碳纖維復合飛輪轉子，進行了高速旋轉狀態下的應力分析，建立了靜力學解析模型，並結合i - deas有限元分析軟體模擬模擬了不同工藝方式的碳纖維復合飛輪轉子的相關幾何參數及工藝參數對其應力水平的影響； 3
  20. Active vibration control technique is the key technology of designing of attitude control system for large flexible spacecraft to fulfill mission requirements such as precision pointing and integrity of structures

    航天器撓性結構的主動振動控制技術是大型航天器姿態控制系統設計的關鍵技術。
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