解消軸 的英文怎麼說
中文拼音 [jiěxiāozhóu]
解消軸
英文
null axis-
Both the methods for measuring such optical constants as cleavage angle, interference color level, extinction angle, length sign, optical sign, optic angle, pleochroism formula, absorptivity formula and the determining program for transparent minerals will be emphasized to lecture
重點講授透明礦物解理夾角、消光角、延性符號、干涉色級序、光性符號、光軸角、多色性公式、吸收性公式的測定方法和透明礦物的鑒定程序。Especially, the idea of " datum dimension precision back " is being put forward, and this idea is being realized by backing composition composed by outer - diameter micrometer, airproof shafting, microwatch. at the same time, use " non - lock " to replace " lock ", this way make the system compact, eliminate many bigger error and resolve th
尤其是提出了基準尺調整后精確後退的思想,並通過外徑百分尺、密珠軸系、千分表組成後退機構加以實現。同時以「無鎖」代「鎖」 ,使系統結構緊湊,受力小,消除了多項較大誤差從而解決了測試精度低的關鍵問題。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。Through calculation on varied parameter, a group of suitable parameter is found out. the results of experiments indicate that the theoretical analysis to the magnetic field of the magnetic structure is proper. to remove the result error come from the change of gap between piston rod and sensor, a signal processing method accompanied with machine learning process is researched
為消除傳感器與磁性標尺之間間隙變化對測量結果的干擾,將示教學習方法引入行程傳感液壓缸的信號處理過程,並使用改進的遺傳演算法解決自學習過程中周期曲線的擬合問題,提出了雙傳感器軸向直線布置方法和基於自學習過程的信號處理方法,通過實驗,達到了顯示精度0 . 01mm ,測量重復精度0 . 2mm的良好效果。According to this structure, a de - coupled microgyroscope is designed, and the simulation results indicated that this three spring - mass structure can effectively eliminate the coupling effects between the drive and sense mode
依據這種結構,設計了一種解耦型微陀螺,模擬結果表明,這種結構基本消除了垂直軸間的機械耦合,降低了對工藝精度和檢測電路的要求。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。分享友人