提出一種對(duì)高速轉(zhuǎn)子軸心位移非接觸測(cè)量的差動(dòng)電感式傳感器結(jié)構(gòu),分析了傳統(tǒng)電橋檢測(cè)電路的不足,設(shè)計(jì)了一種基于“比率脈寬”調(diào)制解調(diào)信號(hào)檢測(cè)電路對(duì)測(cè)量誤差進(jìn)行補(bǔ)償,在此基礎(chǔ)上對(duì)所研制的傳感器的靜態(tài)、動(dòng)態(tài)性能進(jìn)行了測(cè)試。在控制力矩陀螺上進(jìn)行初步試驗(yàn),試驗(yàn)結(jié)果表明:該傳感器能滿足航天器姿態(tài)控制關(guān)鍵執(zhí)行部件長(zhǎng)壽命電磁軸承高速轉(zhuǎn)子軸心檢測(cè)的性能要求。
關(guān)鍵詞:控制力矩陀螺;電磁軸承;位移傳感器

Abstract :On the basis of analyzing the shortage of in2 specting circuit of t raditional elect ric bridge , a sensor st ructure of differential inductance style for non2tangent measuring axes displacement of high speed rotor is pro2 posed. An inspecting circuit with modulated and demod2 ulated signal based on ratio pulse width is designed to compensate for measuring error. The static and dynamic characteristic of developed sensor are tested and primary
experiment is made on CMG( Cont rol Moment Gyro2 scope) . The result shows that the developed sensor can meet the requirement of axes measuring for high speed rotor of active magnetic bearings with long life which is a key performing component for attitude cont rol of space crafter.
Key words :cont rol moment gyroscope ; active magnetic bearing ;displacement sensor