minimum altitude 中文意思是什麼

minimum altitude 解釋
低空
  • minimum : n (pl minimums ma ) 最小,最低,最少限度;【數學】極小(值)。 the irreducible minimum 無法減少...
  • altitude : n. 1. 高,高度;海拔(高度)。2. 【天文學】地平緯度。3. 〈常 pl. 〉高處。4. 高位,高等。5. 【數學】頂垂線,高線。
  1. Mra minimum reception altitude

    最低受信高度
  2. Aom tells very instrument pilot under what visibility ( in terms of runway visual range ( rvr ) ) and or cloud ceiling can the aircraft take off, and under what visibility ( again in terms of rvr ) and visual reference can the aircraft continue the approach to land from the decision altitude ( for precision approaches, e. g. instrument landing system ( ils ) ) or from the minimum descent altitude ( for non - precision approaches ). there are a number of factors affecting the values of aom

    機場最低飛行條件讓每名按儀表駕駛的飛行員知道,航空器在什麼能見度以跑道能見距離來說及或雲幕高度下才可起飛;以及航空器在什麼能見度以跑道能見距離來說及目視基準下,才可從決斷高度用於如使用儀表著陸系統的精確進場或最低下降高度用於非精確進場繼續進場著陸。
  3. New features such as conflict alert and minimum safe altitude warning ( msaw ) systems are provided to further enhance flight safety

    這系統亦加設一些最新的功能,例如沖突警報和最低安全高度警告系統( msaw ) ,以提高飛行的安全性。
  4. In this paper, author briefly introduces some comprehension of his own researches in radar data processing which involves mono - radar trace processing, multi - radar data fusing, short term conflicting alert and minimum safety altitude warning

    本文簡要介紹了本人對雷達數據處理研究的一些理解,對單雷達跟蹤,多雷達融合、短期沖突告警和低高告警的一些原理進行了闡述。
  5. Check your minimum and critical altitude

    檢查你的最低標準和警告高度。
  6. Msa - minimum safe altitude

    最低安全高度
  7. Msa minimum safe altitude

    最低安全高度
  8. Descend to your minimum altitude if not broken contact pull up and go around

    下降到你的最低高度,如不能見,復飛。
  9. Descend to your minimum altitude, if the runway is not in your sight, pull up and go around

    下降到你的最低高度,如看不到跑道,拉起復飛。
  10. The study results show that the minimum ac flashover voltage decreases with the increase of the ice amount accreted on the insulator surface by an exponential law, and the down - trend of the minimum ac flashover voltage will slow gradually with the bridging of the shed of the insulators by icicles, both the average saturated ice amount and the special exponent m of effect of ice amount for different insulators depend on the radius of shed and the air - gaps of the sheds of the insulators, and that the ac ice flashover voltage decrease with the decrease pressure ratio p / p0 ( rise of the altitude ) by power - law for different esdd and icing - states when the altitude is from 4000m to 5500m. the special exponent n, which show the effects of altitude on the flashover voltage, is various with the type of insulator, icing - states and the surface status of iced insulator etc., and that the minimum ac flashover voltage of iced insulators decreases by power - law with esdd or the freezing water conductivity for different ice amount and atmospheric

    研究結果表明:在不同海拔高度和等值鹽密esdd下,絕緣子的最低交流冰閃電壓均隨覆冰量的增加而呈指數規律降低;當覆冰量增加到一定程度后,最低交流冰閃電壓隨覆冰量增加而降低的趨勢趨于飽和;不同絕緣子串的平均飽和覆冰量及閃絡電壓的覆冰量影響特徵指數m均與絕緣子的盤徑和傘距等因素有關;在海拔4000 5500m之間,不同等值鹽密esdd和覆冰狀態下,絕緣子的交流冰閃電壓隨海拔高度的增加(氣壓的降低)與p / p0呈乘冪關系降低,氣壓影響特徵指數n與絕緣子類型、覆冰類型、覆冰表面狀況等因素有關;當覆冰量和氣壓一定時,絕緣子的最低冰閃電壓均隨著等值鹽密( esdd )或覆冰水電導率的增加而呈乘冪關系降低,並逐漸趨于飽和。
  11. The contribution of the paper can conclude as following : according to the laboratory investigations carried out on the ac flashover performance of two types of porcelain insulators and four types of composite insulators at the atmospheric environment of low pressure at a high altitude with pollution and icing, the relations between the minimum ac flashover voltage and the ice amount, the atmospheric pressure as well as the contamination level are obtained

    本文研究的主要工作和結論如下:根據不同絕緣子在人工氣候室內模擬海拔3500m以上低氣壓下覆冰和污穢共存環境中的交流閃絡特性的試驗研究結果,得出了最低閃絡電壓與覆冰量、海拔(低氣壓)和污穢度等因素之間的規律。
  12. Moca minimum obstruction clearance altitude

    最低障害物間隔高度
  13. Simulation results presented here demonstrate that during accelerating flight at constant altitude thrust increases up to approximately 12 percent in the maximum thrust mode, and at subsonic cruise specific fuel consumption decreases up to 2 percent in the minimum fuel consumption mode

    試驗結果表明兩種優化模式下,飛推綜合控制的優化演算法可以顯著提高發動機性能,也驗證了該優化計算機設計方案是可行的。
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