Lunar Orbiter(月球軌道器)到底是什麼？
Lunar Orbiter 月球軌道器 - The first manned landing was also preceded by a series of lunar orbiting satellites and soft landers, the Lunar Orbiter and the Surveyors. [1] Since all communications have to go via a lunar orbiter, all commands and telemetry/data will have to be forwarded to/from the mothership. [2] It is applied to predict the motion of artificial satellites for the two test cases: a lunar orbiter and a satellite of 433 Eros asteroid. [3] The Chang’E-2 (CE2) lunar orbiter was the second robotic orbiter of the Chinese Lunar Exploration Program, as well as the pioneer robotic orbiter in the soft landing project in the second phase of the program. [4]在第一次載人著陸之前，還有一系列月球軌道衛星和軟著陸器、月球軌道飛行器和測量者號。 [1] 由於所有通信都必須通過月球軌道器進行，所有命令和遙測/數據都必須轉發到/從母艦轉發。 [2] 它用於預測人造衛星的運動，用於兩個測試案例：月球軌道器和 433 Eros 小行星的衛星。 [3] 嫦娥二號（CE2）月球軌道飛行器是中國探月計劃第二個機器人軌道飛行器，也是該計劃二期軟著陸工程的先驅機器人軌道飛行器。 [4]
Pathfinder Lunar Orbiter 探路者月球軌道器
The suggested sites may be further re-examined by the Korean Pathfinder Lunar Orbiter during the nominal 1-year mission period in 2021. [1] In this study, the observational arc-length effect on orbit determination (OD) for the Korea Pathfinder Lunar Orbiter (KPLO) in the Earth-Moon Transfer phase was investigated. [2]韓國探路者月球軌道器可能會在 2021 年標稱的 1 年任務期內進一步重新檢查建議的地點。 [1] 在這項研究中，研究了地月轉移階段韓國探路者月球軌道器（KPLO）的觀測弧長對軌道確定（OD）的影響。 [2]
lunar orbiter laser 月球軌道器激光器
They can be tracked by an orbiting laser altimeter, such as the Lunar Orbiter Laser Altimeter, from a distance of a few hundred kilometers or by a landing lidar on future lunar landers. [1] the high-resolution Lunar Orbiter Laser Altimeter (LOLA) digital elevation map [8]), TA-JDR can be used to localize a user with greater accuracy than just the standard JDR-LOC. [2] For the detection and mapping of rilles, we used images from the Lunar Reconnaissance Orbiter Camera (LROC) [1] which have a resolution of 100 m/pixel and the DEM from Lunar Orbiter Laser Altimeter (LOLA) with a resolution of 6 m/pixel. [3] In this paper, we propose a Moon-based Earth observation intervisibility algorithm, based on the Lunar Orbiter Laser Altimeter (LOLA) data. [4] The inclusion of available Lunar Orbiter Laser Altimeter (LOLA) shots as 3D ground control to the BA, accurately tied to the image space by an aforegoing co-registration, allowed to register the final adjusted NAC DTM to the currently most accurate global lunar reference frame. [5] The lunar surface is modeled by Digital Elevation Model (DEM) data from Lunar Reconnaissance Orbiter (LRO) Lunar Orbiter Laser Altimeter (LOLA). [6] Previous study of this area using data from the Lunar Orbiter Laser Altimeter (LOLA), Diviner and LAMP instruments aboard Lunar Reconnaissance Orbiter (LRO) shows a spatial correlation between brighter 1064 nm albedo, annual maximum surface temperatures low enough to enable persistence of surface water ice ( We find features in far-IR emissivity (50–400 μm) could be attributed to either, or a combination, of two effects (i) differential regolith emissive behavior between permanently-shadowed temperature regimes and those of normally illuminated polar terrain, perhaps related to presence of water frost (as indicated in other studies), or (ii) high degrees of anisothermality within observation fields of view caused by doubly-shaded areas within the PSR target that are colder than observed brightness temperatures. [7] We developed a reasonable data processing method based on all of the valid Lunar Orbiter Laser Altimeter (LOLA) data and produced an improved DEM of the Mons Rumker region. [8] To evaluate the effectiveness and robustness of the proposed method, experiments were conducted on three lunar scenes using both orthoimages from the Lunar Reconnaissance Orbiter (LRO) and DEM data acquired by the Lunar Orbiter Laser Altimeter (LOLA). [9] The 1,064‐nm laser reflectance measurements collected by the Lunar Orbiter Laser Altimeter (LOLA) onboard the Lunar Reconnaissance Orbiter (LRO) provide a unique opportunity to detect and characterize PSR water ice. [10] 6$^\circ$N) model based on the elevation data obtained from the Lunar Orbiter Laser Altimeter onboard Lunar Reconnaissance Orbiter (LRO), and then calculated the distribution of the effective solar irradiance at different local times. [11] A case study with the Lunar Orbiter Laser Altimeter (LOLA) crater map (Head et al. [12]它們可以被軌道激光高度計（如月球軌道器激光高度計）從幾百公里的距離或未來月球著陸器上的著陸激光雷達跟踪。 [1] 高分辨率月球軌道飛行器激光高度計 (LOLA) 數字高程圖 [8]），TA-JDR 可用於定位用戶，比標準 JDR-LOC 更準確。 [2] 對於小溪的探測和繪圖，我們使用了分辨率為 100 m/像素的月球勘測軌道器相機 (LROC) [1] 的圖像和分辨率為 6 m/像素的月球軌道器激光高度計 (LOLA) 的 DEM像素。 [3] 在本文中，我們提出了一種基於月球軌道器激光高度計（LOLA）數據的基於月球的地球觀測可觀測性算法。 [4] 包含可用的月球軌道器激光高度計 (LOLA) 鏡頭作為 BA 的 3D 地面控制，通過上述配準準確地綁定到圖像空間，允許將最終調整的 NAC DTM 配準到當前最準確的全球月球參考框架. [5] 月球表面由來自月球勘測軌道器 (LRO) 月球軌道器激光高度計 (LOLA) 的數字高程模型 (DEM) 數據建模。 [6] 先前使用月球軌道飛行器激光高度計 (LOLA)、占卜器和月球勘測軌道器 (LRO) 上的 LAMP 儀器的數據對該區域進行的研究表明，較亮的 1064 納米反照率與年最高表面溫度之間的空間相關性足夠低以使地表水能夠持久存在冰（我們發現遠紅外發射率（50-400μm）的特徵可以歸因於兩種效應中的一種或兩種效應的組合（i）永久陰影溫度狀態和正常光照極地地形之間的差異風化層發射行為，可能與水霜的存在有關（如其他研究所示），或 (ii) 由 PSR 目標內的雙陰影區域引起的觀察視野內的高度不等溫性比觀察到的亮溫更冷。 [7] 我們基於所有有效的月球軌道飛行器激光高度計 (LOLA) 數據開發了一種合理的數據處理方法，並產生了 Mons Rumker 地區的改進 DEM。 [8] 為了評估所提出方法的有效性和魯棒性，我們使用來自月球勘測軌道器 (LRO) 的正射影像和月球軌道器激光高度計 (LOLA) 獲取的 DEM 數據對三個月球場景進行了實驗。 [9] 月球勘測軌道器 (LRO) 上的月球軌道器激光高度計 (LOLA) 收集的 1,064 nm 激光反射率測量結果為探測和表徵 PSR 水冰提供了獨特的機會。 [10] 6$^\circ$N) 模型基於月球勘測軌道飛行器（LRO）上的月球軌道飛行器激光高度計獲得的高程數據，然後計算出不同當地時間的有效太陽輻照度分佈。 [11] 月球軌道飛行器激光高度計 (LOLA) 隕石坑地圖的案例研究（Head 等人。 [12]