导弹与航天运载技术
導彈與航天運載技術
도탄여항천운재기술
Missiles and Space Vehicles
2015年
6期
103-106
,共4页
王振兴%贺长水%高明杰%贺永喜
王振興%賀長水%高明傑%賀永喜
왕진흥%하장수%고명걸%하영희
倾角仪%零点标定%温域补偿
傾角儀%零點標定%溫域補償
경각의%영점표정%온역보상
Inclinometer%Zero point calibration%Temperature scope compensation
设计一种精密倾角仪,采用零位标定确定倾角仪的准确零点位置,并提出一种温域补偿的实现方法.建立倾角仪的输出模型,采用两位置法对倾角仪进行零位标定;建立多项式误差模型,采用曲线拟合的方式对倾角仪的测量误差进行温域补偿.经过试验验证,倾角仪在-40~+60℃温度范围,-30~+30°角度范围内的测量误差绝对值达到了不大于30″的精度.该倾角仪可在快速、大角度、宽温域倾角的测量上进行应用.
設計一種精密傾角儀,採用零位標定確定傾角儀的準確零點位置,併提齣一種溫域補償的實現方法.建立傾角儀的輸齣模型,採用兩位置法對傾角儀進行零位標定;建立多項式誤差模型,採用麯線擬閤的方式對傾角儀的測量誤差進行溫域補償.經過試驗驗證,傾角儀在-40~+60℃溫度範圍,-30~+30°角度範圍內的測量誤差絕對值達到瞭不大于30″的精度.該傾角儀可在快速、大角度、寬溫域傾角的測量上進行應用.
설계일충정밀경각의,채용령위표정학정경각의적준학영점위치,병제출일충온역보상적실현방법.건립경각의적수출모형,채용량위치법대경각의진행령위표정;건립다항식오차모형,채용곡선의합적방식대경각의적측량오차진행온역보상.경과시험험증,경각의재-40~+60℃온도범위,-30~+30°각도범위내적측량오차절대치체도료불대우30″적정도.해경각의가재쾌속、대각도、관온역경각적측량상진행응용.
In this paper, a precision inclinometer which used zero calibration to demarcate the accurate aero point position of the inclinometer was designed and the implementation method of temperature scope compensation was put forward. The output model of inclinometer was established and two location methods were used to demarcate the zero point position. A polynomical error model was established and curve fitting method was adopted to realize the temperature scope compensation of the inclinometer measurement error. The test result showed that the inclinometer measurement error's absolute value less th″an 30 when applied in-40~+60℃ temperature range and-30~+30°range. This inclinometer can be used on rapid、large angle、wild temperature scope measurement.