flying formation 中文意思是什麼

flying formation 解釋
飛行編隊
  • flying : adj 1 飛的，飛行的，飛行員的。2 飄揚的，飛舞的。3 飛似的，飛速的。4 臨時的，短暫的。5 到處流傳的...
  • formation : n. 1. 構成，形成；設立；編制。2. 組織，構造；形態；形成物，構造物；【軍事】編隊，隊形；兵團。3. 【地質學；地理學】層；組； 【生物學】社區；（植物）群系。adj. -al
  1. My cosmopolite was sustaining the pride and reputation of the earth when the waiters closed in on both combatants with their famous flying wedge formation and bore them outside, still resisting

    我的世界公民仍保持著地球的驕傲和名聲，就在這時，侍者們利用著名的飛速楔形結構插入兩個格鬥者之間，硬把他兩個推出了咖啡館，盡管還在抵抗。
  2. The concept of satellite formation flying has provided new application directions and developable space for small satellites, and has received much attention

    衛星編隊飛行這一概念的提出，為小衛星開辟了新的應用方向和發展空間，受到國內外學者的普遍關注。
  3. This paper is to study the relevant issues of satellite formation flying from the point of view of dynamics and control

    本文從動力學和控制的角度出發，對衛星編隊飛行進行了有益的探索和研究。
  4. For example, it can be used to drag make - up and solar pressure cancellation of low orbit spacecraft, formation flying and precise positioning of small satellite, repos

    同時， mpt也可用於低軌道（ 300 500km ）航天器的大氣阻力補償，星際航行航天器的主推進，以及星座和小型衛星的編隊飛行和精確定位等，具有廣闊的應用前景。
  5. Relative orbit configuration for satellite formation flying

    衛星編隊飛行中的相對軌道構形
  6. Autonomous relative orbit determination for satellite formation flying on basis of orbit element differences

    基於軌道根數差的衛星編隊自主定軌研究
  7. Satellite formation flying on elliptic orbits is studied in this thesis

    對橢圓軌道上的衛星編隊飛行的進行了研究。
  8. Kinematic models of formation flying constellation and configuration design

    編隊飛行星座相對運動的運動學描述與編隊構型設計
  9. Examples of this type of control include formation flying, instrument flight, and landing.

    這類操縱的例子包括編隊飛行，儀表飛行和著陸。
  10. The fighter planes, flying in formation, one by one peeled off to left and right

    編隊飛行的戰斗機一架地向左右兩邊飛離編隊。
  11. He was flying in formation with eleven other jets

    他跟另外十一架噴射機以隊形飛行。
  12. The generalization of the work will provide theoretical foundation and guiding for the multistatic radar system and formation flying of space based radar

    有關工作的推廣將為多基地雷達系統和星載雷達的編隊飛行方案提供理論基礎和指南。
  13. Based on the first order perturbing solutions, the thesis obtained the long term relative perturbation of equal semi - major axis formation, which is removed by adjusting semi - major axis of the flying - around satellite

    接著，基於一階攝動解，得出了等半長軸繞飛編隊的長期相對攝動規律，並通過調整環繞衛星的半長軸消除了長期相對攝動。
  14. Much attention is paid to the effect of perturbations on satellite formation flying and how to decrease the effect, which are studied with the earth oblateness and atmospheric drag considered

    攝動因素對衛星編隊飛行的影響以及如何盡量減小攝動影響是應用中非常關心的問題，本文考慮地球扁率和大氣阻力兩種攝動因素，對此進行了研究。
  15. Based on the two - body assumption, two methods are used to investigate the mechanism of satellite formation flying on circular or near - circular orbits

    首先基於二體假設，採用兩種方法系統地研究了圓或近圓軌道上衛星編隊飛行的構成機理。
  16. Based on the first order perturbing solutions due to the earth oblateness, the long term relative perturbation of equal semi - major axis formation is analyzed, which is removed by adjusting semi - major axis of the flying - around satellite

    在地球扁率攝動一階解的基礎上，分析了等半長軸編隊飛行的長期相對攝動規律，並提出了消除長期相對攝動的編隊設計方法，即調整環繞衛星的半長軸。
  17. The primary studies on the methods that use small satellites flying in formation to implement global 3d measurements are developed in order to provide some valuable reference for the researches of the space - based integrated information network

    對用小衛星編隊飛行進行全球地形三維測量方法進行初步研究，希望能對我國天基綜合信息網方面的研究有一定的參考價值。
  18. Several schemes, which use small satellites flying in formation to acquire global three - dimensional imaging, are also proposed in this dissertation, followed by the analysis and selection of the system parameters of one of the three small satellites

    論文提出用小衛星編隊飛行實現全球三維成像的幾種方案，並對一種三星方案的系統參數進行了詳細的分析和選擇。
  19. The third chapter involves some problems on attitude determination and integrity ambiguity resolving. using three formation flying satellites for an earth observation as an example, the forth chapter contains some problems about determination of inter - satellite position, attitude and time, by using high precise pseudo - ranging observation onboard pseudolites. the problems are the selecting of coordinate system and independent state parameters, the setting of observation equations, and the conversion of constellation ' s states

    第四章以三星編隊星座為例，討論利用擴展的高精度星間偽距觀測進行星間相對位置、姿態和時間參數確定的一些問題，包括：坐標系、獨立參數的選取、觀測方程的建立和星座狀態的轉換等。
  20. In the end, a kind of fully distributed coordination strategy for the relative control of formation flying satellites is given. finally, based on the coordination strategy mentioned above, considering the

    模擬結果表明，這兩種控制律能夠在存在各種干擾力矩及衛星模型的不確定性的情況下，有效地提高編隊衛星相對姿態控制精度。
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