multi-orbit 中文意思是什麼

multi-orbit 解釋
多軌道的
  • multi : 並聯的,多路系統
  • orbit : n 1 【天文學】軌道;【解剖學】眼窩,眶;(鳥或昆蟲的)復眼緣的頰部。2 (人生的)旅程,生活過程;...
  1. Based on the theory of software architecture, the hierarchical structure is used for designing the software system because the aocs demands real - time and high reliability. the integrated environment for software cross - development of vxworks is used for simulating the schedule of several multi - tasks, the managing of work mode and the communication among the modules. an approach of software architecture for the attitude and orbit control system of satellite is developed in this paper, which is based on a deep study and analysis of modern software techniques

    本文運用軟體體系結構的理論,通過對多種軟體體系結構的分析比較,針對衛星姿軌控系統實時、高可靠、復雜等特點,採用層次結構方案進行了體系結構設計,並運用實時操作系統vxworks的集成開發環境,完成了姿軌控系統多任務調度管理、工作模式管理和應用模塊間相互通信的模擬實踐。
  2. Launched by a multi - stage ares 5 rocket, the spacecraft will go into orbit around the earth before docking with the international space station

    太空船被多級阿瑞斯5號火箭發射,在泊入國際空間站之前將進入環地軌道。
  3. The soviet union launches the voskhod 1 into earth orbit as the first spacecraft with a multi - person crew and the first flight without space suits on october 12

    1964年10月12日,蘇聯發射日出一號進入地球軌道。日出一號是第一艘運載多名宇航人員並且無一著太空服的太空船。
  4. The advantages of using leo satellite are as following : on the one hand the satellite orbit is low, so the transmission delay is short, the power loss is small ; on the other hand the development of cell communication, multi - access, frequency multiplex and etc also provide a technique guarantee to the leo satellite - mobile - telecommunication. so the leo system is considered to be a satellite - mobile - communication system with a great future

    低軌道衛星是一種運行於1000公里左右的高空中的人造衛星,利用leo衛星實現個人通信的優點在於:一方面衛星的軌道高度低,使得傳輸延時短、路徑損耗小,多個衛星組成的星座可實現真正的全球覆蓋,頻率復用更有效:另一方面蜂窩通信、多址、點波束、頻率復用等技術的發展也為低軌道衛星移動通信提供了技術保障。
  5. At the point of co = g > c, it is the hopf bifurcation that the rotor orbit of shaft centerline is the periodic whirl of small amplitude. the method is suitable for the multi - freedom system

    數值求解系統動力學方程,在_ c處,轉子軸心軌跡為極小幅值的周期渦動,此為hopf分岔,分叉后,系統運動為擬周期運動。
  6. The theories of multi member function ' s extremity value, hooke jeeves mode searching method solving wholly complex problem of extremity value and uniformity design method, one new and efficient method to choose test point, are applied to establish the two - dimension oil well orbit optimized model. the shortest length of oil well orbit curve is regarded as this model ' s object and all kinds of effecting parameters are analyzed

    通過引入多元函數極值理論、求解復雜極值問題的hookejeeves模式搜索法及一種較為新穎和高效的試驗點選擇方法:均勻設計法,建立以最短油井軌跡曲線長為目標的二維油井軌道優化設計模型,並對影響井軌跡曲線的參數進行了較為詳細的分析。
  7. The space observation in soft x - ray and extreme ultraviolet ( euv ) region is an important portion of the space astronomy and an effective solar observation method developed increasingly. in this thesis we designed a euv multi spectrum space solar telescope ( eut ) based on the requirement of high angular resolution and wide field of view for solar observations ; investigated the transmission performance of eut ; invented a method of eut pointing calibration on the space orbit and solved the high precision pointing calibration problems ; constructed a prototype of 17. 1nm telescope, tested the possibility of eut design, and developed some cutting - edge techniques

    本文根據空間平臺上高解析度對日觀測的需要,設計出一種可以在四個極紫外波段對日同時成像多光譜太陽望遠鏡( eut ) ;研究了極紫外( euv )波段太陽望遠鏡光學傳輸特性;提出了真空紫外波段在軌指向的標定方法,解決了高精度指向標定問題;研製出一臺17 . 1nm望遠鏡的地面樣機,驗證eut設計的可行性,攻克了部分關鍵的技術難關;為進一步的研究工作奠定了基礎。
  8. Firstly, with the help of angular momentum coupling theory, the hamiltonian for multi - electron adorns is rewritten in terms of spherical tensors. the advantage of this form is that the radial, angular and spin parts are separated completely, which makes it easy to calculate the angular matrix elements by means of irreducible tensor. secondly, theoretical expressions of the relativistic corrections including the relativistic mass correction, the darwin correction terms, the electron - electron contact terms and the orbit - orbit interaction which contribute to the non - relativistic energy for two - electron atom are theoretically derived in the lsmlms scheme

    具體內容包括:首先,藉助角動量耦合理論,將多電子原子哈密頓算符中的自旋-自旋、自旋-其它軌道以及軌道-軌道相互作用全部改用球張量表示,這種球張量形式的優點在於已將原子哈密頓算符中的徑向、角向和自旋部分完全分開,從而便於計算矩陣元,而且角向矩陣元可以方便地利用不可約張量理論來進行計算。
  9. This paper is divided to 3 parts and provides a detailed discuss on formatting fly technology in chapter 3, 4, 5 respectively : chapter 3 provides a method for formatting orbit design, chapter 4 researches on a multi - agent based satellite on - board management system, chapter 5 focuses on a wireless token bus protocol, simulates the protocol and analysis the simulating result

    本文主要分為3個專題在三、四、五章對衛星編隊技術進行了詳細的闡述。其中,在第三章主要對衛星編隊構型及軌道設計作了深入的專題研究。第四章提出了一種基於multi - agent技術的編隊小衛星星務管理系統。
  10. Multi - orbit tomographic unit

    多軌跡斷層攝影機
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