guidance sensitivity 中文意思是什麼

guidance sensitivity 解釋
制導靈敏度
  • guidance : n. 1. 向導，指引，指導。2. 導航；制導。3. 【機械工程】導槽，導板，導管。
  • sensitivity : n. 1. 敏感（性）；感受性。2. （儀器等的）靈敏性。3. 【攝影】感光度。
  1. Sensitivity of guidance error of tv - guided missile based on orthogonal experiments

    基於正交試驗的電視制導空地導彈制導誤差靈敏度分析
  2. Currently in use is more slimming products appetite inhibitors, should be used to its side effects, which normally takes the doctor used under the guidance of the drug, side effects and dosage of the drug, the greater the dose the greater side effects, while each pair of drug sensitivity not the same and thus should start small dose and gradually to increase the effective dose ; during another drug not suddenly interrupted, it should gradually decrease until suspended medication before or during inspection as biochemical blood glucose and lipids, weight monitoring and, if necessary, timely adjust dosage

    目前所用的減肥藥多是食慾抑制劑，使用應注意其副作用，一般需在醫生的指導下服用，藥物的副作用與藥物劑量有關，藥量越大副作用也越大，同時每個人對藥物的敏感性也不一樣，因而應從小劑量開始，逐漸增加劑量至有效；另外用藥期間不能突然中斷，也應逐漸減量直至停用，服藥前或期間檢查血生化如血糖、血脂，監測體重，必要時及時調整用藥量。
  3. Take certain typed three compartment sedan as an example, on the basis of simulation calculation of torsional rigidity and by applying the finite element theory and through sensitivity analysis of torsional rigidity via board thickness of part this paper gained the key frame structure that affects the torsional rigidity of white body and under the guidance of this frame structure the measures of further enhancing its torsional rigidity was laid down for the being studied sedan pattern

    以某型三廂轎車為例，在扭轉剛度模擬計算的基礎上，應用有限元理論，通過零件板厚對扭轉剛度的靈敏度分析，得到了影響白車身扭轉剛度的關鍵框架結構，並在此框架結構的指導下，對所研究車型制定了進一步提高其扭轉剛度的措施。
  4. At the same time, h guidance law of the air - air missile is designed with l2 gain theory and the h2 / hx mixed control theory to minish the sensitivity to maneuverable goal

    同時基於不確定非線性系統的幾增益理論和h : / hao混合控制理論研究了空一空導彈的h 』魯棒制導律的設計，以減小空一空導彈制導律對目標機動的敏感性。
  5. The tactical missile seeker handover accuracy from midcourse to terminal guidance is researched. the small perturbation method is proposed to analyse error sensitivity of the seeker presetting parameters from error sources. firstly, the terminal guidance seeker presetting parameters are computed, based on the equations of a surface - to - air missile movement and a target movement. then the seeker presetting unaccuracy due to the command guidance radar measurement errors is also computed. it can be seen that the seeker presetting errors increase rapidly when the missile is close to the target, which leads to an important conclusion that the late seeker handover from midcourse to teminal guidance should be avoided

    研究復合制導的戰術導彈中末制導交班的導引頭預定精度問題.提出用小擾動法分析導引頭預定參數對誤差源的誤差敏感性關系.以中遠程防空導彈為例，結合導彈運動方程組和目標運動模型，計算了中末制導交班的導引頭預定參數，並計算了在制導站雷達測量誤差下的末制導導引頭預定參數的計算精度.可知，導引頭定位參數的計算誤差隨著彈目距離的接近而顯著增大，得到中末制導交班不能太晚的重要結論
  6. Abstract : the tactical missile seeker handover accuracy from midcourse to terminal guidance is researched. the small perturbation method is proposed to analyse error sensitivity of the seeker presetting parameters from error sources. firstly, the terminal guidance seeker presetting parameters are computed, based on the equations of a surface - to - air missile movement and a target movement. then the seeker presetting unaccuracy due to the command guidance radar measurement errors is also computed. it can be seen that the seeker presetting errors increase rapidly when the missile is close to the target, which leads to an important conclusion that the late seeker handover from midcourse to teminal guidance should be avoided

    文摘:研究復合制導的戰術導彈中末制導交班的導引頭預定精度問題.提出用小擾動法分析導引頭預定參數對誤差源的誤差敏感性關系.以中遠程防空導彈為例，結合導彈運動方程組和目標運動模型，計算了中末制導交班的導引頭預定參數，並計算了在制導站雷達測量誤差下的末制導導引頭預定參數的計算精度.可知，導引頭定位參數的計算誤差隨著彈目距離的接近而顯著增大，得到中末制導交班不能太晚的重要結論
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