航空兵器
航空兵器
항공병기
HANGKONG BINGQI
2012年
6期
50-52,61
,共4页
数学模型%部件调试%取值区间%仿真
數學模型%部件調試%取值區間%倣真
수학모형%부건조시%취치구간%방진
mathematics model%component adjustment%approximate value range%simulation
对某型导弹温度测量部件的工作原理进行了分析，建立了该部件全温度数学模型。根据数学模型对该部件的调试电阻阻值分布进行了计算机仿真，确定了调试电阻的取值区间。利用一次试配调试电阻的全温测试数据，通过仿真预算出调试电阻的精确阻值，指导该部件的调试，提高调试效率。
對某型導彈溫度測量部件的工作原理進行瞭分析，建立瞭該部件全溫度數學模型。根據數學模型對該部件的調試電阻阻值分佈進行瞭計算機倣真，確定瞭調試電阻的取值區間。利用一次試配調試電阻的全溫測試數據，通過倣真預算齣調試電阻的精確阻值，指導該部件的調試，提高調試效率。
대모형도탄온도측량부건적공작원리진행료분석，건립료해부건전온도수학모형。근거수학모형대해부건적조시전조조치분포진행료계산궤방진，학정료조시전조적취치구간。이용일차시배조시전조적전온측시수거，통과방진예산출조시전조적정학조치，지도해부건적조시，제고조시효솔。
By analyzing the working principle of the missile temperature measurement component, a mathematics model of the component in the full temperature range is established. Based on this model the value distribution of the component' s adjustable resistance is simulated, and the approximate value range of the adjustable resistance is defined. Using the full temperature test data of the adjustable resistance in preassembly, the precise value of the adjustable resistance can be calculated. The mathematics model has instructional signification on the component adjustment, and it can improve the assembly efficiency.
