行星軌道 的英文怎麼說

中文拼音 [hángxīngguǐdào]
行星軌道 英文
orbit n. 名詞 the path of one heavenly body round another
  • : 行Ⅰ名詞1 (行列) line; row 2 (排行) seniority among brothers and sisters:你行幾? 我行三。where...
  • : 名詞1 (夜晚天空中閃爍發光的天體) star 2 [天文學] (宇宙間能發射光或反射光的天體) heavenly body...
  • : Ⅰ名詞1. (路軌;軌道) rail; track 2. (比喻辦法、規矩、秩序等) rut; path; course Ⅱ動詞[書面語] (遵循; 依循) follow
  • : Ⅰ名詞(道路) road; way; route; path 2 (水流通過的途徑) channel; course 3 (方向; 方法; 道理) ...
  • 行星 : [天文學] planet
  • 軌道 : 1 (供火車、電車等行駛的由條形鋼材鋪成的路線) track; pathway; rail; runway; circle; railway 2 (...
  1. Because it ’ s hard to get radiation - harden hardware overseas, so the software fault tolerance techniques are significant for our national space enterprise. the computer platform of 863 plan project ” micro intelligent free - flying space robotic system ” consists of cots component. the orbit and the radiation environment of the robot are similar to ones of the argos satellite, and the system is required to have high reliability. therefore it ’ s necessary to applied the software fault tolerance techniques into the system to improve the anti - radiation capability after the techniques been verified valid

    因為我國很難從國外獲得輻射加固的硬體,所以,這項軟體容錯技術對我國航天事業的發展具有較大意義。 863計劃項目「小型智能飛機器人系統」所用的計算機平臺採用商用器件,其衛的運與argos衛近似,面臨的輻射環境與argos衛相似,要求具有高可靠性。因此,小型智能飛機器人系統有必要在驗證sihft技術有效的基礎上,應用軟體容錯技術,提高其空間抗輻射能力。
  2. Dynamic model of satellite is built up with astronomic method, and a short - arch forecast arithmetic of satellite orbit in short arch with single site is given, which is of high precision when only angle data is available

    本文使用了天文方法建立了人造衛運動的數學模型,給出了一種只使用單站短弧段測角數據對人造衛高精度預測的演算法。
  3. The planets occupy orbits that are regularly spaced according to a pattern first noticed by bode.

    在空間的位置是有一定規則的,波特首先注意到了這種規律性。
  4. So combine the item of “ space targets surveillance photoelectricity telescopes arrays system ”, this thesis does research in developing space targets visualization system. the main achievement in this thesis can be summarized as follows : 1. expatiate e the basic theory of satellite track dynamic, analyse the orbit characteristic of two - body problem and launch window, subastral point calculation, visibility and coverage analysis, two - line element sets

    本文結合「空間目標監視光電望遠鏡陣系統」課題,進了空間目標可視化系統的設計和研究,主要作了以下幾方面的工作: 1 、闡述了衛動力學的基本原理,分析了二體特性和發射窗口的基本特性,下點跡計算、可見性和覆蓋分析和兩根數。
  5. The most feature of the orbits of near - earth asteroids ( neas ) is that the semi - major axes of the orbits are nearly equal to that of the earth or the perihelia distances are approximate to or even less than the mean distance between the sun and the earth, thus they could move into inside of the earth ' s orbit, so that they might close approach or even colliside with the earth ( or other planets, such as the venus, the mars, etc. )

    近地小行星軌道的最大特點是其半長徑與地球半長徑相近,或近日距離接近甚至小於日地平均距離,其運動可深人到地球的內部,這將導致該類小與地球(還有金、火等)十分靠近甚至發生碰撞。
  6. The asteroids are the most important small bodies in the solarsystem, and they mainly lies in the two locations - a main belt between the mars ' s orbit and the jupiter ' s and the near - earth space. the most feature of the orbits of near - earth asteroids ( neas ) is that the semi - major axes of the orbits are nearly equal to that of the earth or the perihelia distances are approximate to or even less than the mean distance between the sun and the earth, thus they could move into inside of the earth ' s orbit, so that they might close approach or even colliside with the earth ( or other planets, such as the venus, the mars, etc. ). the characteristic brings about some difficulties in the numerical research during their orbital evolution, which leads to the failure of the normalization technique in the general removal impact singularities of celestial mechanics methods and the symplectic algorithm which is successfully applied to the investigation in quality. by comparing the computation effects of several common numerical methods ( including symplectic algorithm ), and considering the nature of the movement of the small bodies, the corresponding treatments are provided here to improve the reliability of the computation

    是太陽系最重要的一類小天體,主要分佈在兩個區域;火和木之間的一條主帶和近地空間.近地小行星軌道的最大特點是其半長徑與地球半長徑相近,或近日距離接近甚至小於日地平均距離,其運動可深入到地球的內部,這將導致該類小與地球(還有金、火等)十分靠近甚至發生碰撞.這一特徵給其演化數值研究帶來一些困難,包括天體力學方法中一般消除碰撞奇點的正規化處理以及對定性研究十分成功的辛演算法都將在不同程度上失效.通過對幾種常用數值方法(包括辛演算法)計算效果的比較,根據小天體運動自身的特性,給出了相應處理措施,從而可提高計算結果的可靠性
  7. 1979 america ? s skylab i returned to the earth after 34 981 orbits, since its launch on 14th may 1973

    1973年5月14日發射的美國太空實驗空間站1號,繞衛34 , 981圈后,返回地面。
  8. In the first, this article introduces the knowledge of orbit designing, then this article summarizes the basic methods and principles of orbit designing. in the later, this article describes the conception of node period about orbit designing emphatically which has been advanced by the writer. at the same time, this article describes the process of the writer ' s analysing and designing the orbit of earth spying satellite particularly with the conception. in the last, this article describes the wirter ' s analysing and simulating the designing results

    本文首先介紹了設計的基本知識,然後總結了設計的基本的方法和原則。在隨後部分重點對衛設計中交點周期的概念提出了自己的看法,同時應用此結果詳細分析和設計了對地偵察衛的太陽同步回歸,最後對此設計結果進詳細模擬分析。
  9. Thirdly, an ideal satellite orbit is simulated, and on this foundation, we establish some typical simulation and testing circumstances. lastly, after simulation in the simulation and testing circumstances, we compare the performance of ukf and ekf. and then, based on the outdoor experiment of the vehicle, an analysis and contrast between our simulation results and commercial data process software is carried out, and the conclusion is obtained

    首先在第三章提出的目標運動模型的基礎上建立了系統狀態方程;其次簡要分析了衛導航系統中的各類誤差,建立了基於偽距觀測量的系統觀測模型;第四節利用yuma格式歷書數據模擬了未受攝動影響的衛,並在此基礎上建立了幾種典型的動態模擬測試環境;第五節為模擬分析和比較,先對ukf演算法和ekf演算法在動態模擬測試環境中進了模擬比較,然後針對外場試驗,對非線性濾波獲得的定位結果與商業軟體進了分析比較,並得出結論。
  10. The research uncovered the facts that, in the design of space vehicles, the single event effects induced by high - energy protons and iron ions in space must be taken into account seriously, the proper hardening measures must be taken to protect the electronic devices from disfunction. it is also suggested that, for the low - orbit satellites, the south atlantic anominal zone should be avoided

    宇宙高能質子和鐵離子的單粒子效應在航天任務設計中需要重點考慮,空間應用的電子學元器件,必須進適當的抗輻射加固,在設計低時必須設法避開南大西洋異常區( saa ) ,航天任務設計中還需要掌握太陽質子事件總體上11年為周期的特性。
  11. Each mission had a satellite designed to photograph the surface of mars from orbit, and to act as a communication relay for the viking lander that each mission carried

    每次任務都發射一枚具備從火拍攝火表面能力的人造衛,同時充當與海盜登陸者進聯絡的中間站。
  12. The asteroids are the most important small bodies in the solar system, and they mainly lies in the two locations - a main belt between the mars ' s orbit and the jupiter ' s and the near - earth space

    摘要小是太陽系最重要的一類小天體,主要分佈在兩個區域;火和木之間的一條主帶和近地空間。
  13. The dissertation presents a new method for orbital maneuver based on zero effort miss steering, and many problems in this method are studied

    本文提出了基於零控流型的衛機動方法,並對此方法所涉及的具體問題進了研究。
  14. Here shows the size of the orbits

    下圖顯示了行星軌道的大小。
  15. Most stations are located in orbit around planets, or in ( for mining stations ) in asteroid fields / belts

    多數空間站位於近行星軌道上,采礦站則多設置在小帶中。
  16. Under proposed international astronomical union definitions, two planets that orbit each other around a barycenter between them are a binary planet

    根據國際天文學會的定義提出兩個行星軌道周圍的重心在彼此之間是雙系統。
  17. While the death star was forced to orbit a target world before firing its superlaser and annihilating the planet, the galaxy gun fired giant, high - yield explosive projectiles into hyperspace

    與死在超級激光聚能並開火毀滅目標之前要首先進入並環繞該行星軌道不同,銀河之槍直接向超太空發射出巨大的,高能量爆炸性的發射彈。
  18. Since its launch in 1990 the hubble space telescope has captured beautiful images of the universe, such as the birth of stars in stellar nurseries, while conducting rigorous science, such as the recent detection of planets orbiting stars near the centre of the milky way

    自1990年發射以來,哈勃太空望遠鏡不僅捕捉到了宇宙的美麗景象如在恆溫床中產生的恆,同時也建立了精密的科學理論如近期觀測到了在銀河中心附近沿行星軌道的恆
  19. Though the hill equation was improved it cannot satisfied with the long distance navigation. here is considering the main satellite the following satellite and the target satellite format a triangle in the space which was useful in the relative navigation. the orbit of the following satellite was resolved by calculate the hill equation

    盡管如此改進的hill方程依然不能滿足遠距離的相對導航,當從在攔截目標時,若目標在攔截過程中發生機動遠離主,這里考慮到在已知從的前提下利用主從以及目標在空間形成的三角關系這一有利條件進幾何法定位的研究,並通過數學模擬對其誤差大小進了分析。
  20. Hat - p - 1 orbits one of a pair of distant stars hundreds of light - years beyond ours

    環繞距離我們幾百光年之遙的一對遠距離恆
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