固体火箭技术
固體火箭技術
고체화전기술
JOURNAL OF SOLID ROCKET TECHNOLOGY
2014年
2期
281-284
,共4页
张丹阳%夏云峰%李信元%赵亮
張丹暘%夏雲峰%李信元%趙亮
장단양%하운봉%리신원%조량
柔性喷管%动态摆心测试%激光位移传感器
柔性噴管%動態襬心測試%激光位移傳感器
유성분관%동태파심측시%격광위이전감기
flexible joint nozzle%dynamic test of pivot point%laser displacement sensor
为了开展柔性喷管全轴摆动动态摆心测试,设计了一种以激光位移传感器、测控装置为基础的测试系统。通过建立数学模型,搭建试验测量装置,利用数据采集处理系统得到了动态摆心漂移数据。该系统采用高精度高频响的激光位移传感器保证了动态响应速度,程控调平机构解决了传感器的精确定位问题,软硬件滤波较好地剔除了扰动信号。系统采样频率2 kHz,输出测量数据频率不低于1 kHz;与静态方法相比较,测量相对误差不大于1%。结果表明,该系统能够准确、实时地测试喷管全轴摆动时的摆心漂移轨迹。
為瞭開展柔性噴管全軸襬動動態襬心測試,設計瞭一種以激光位移傳感器、測控裝置為基礎的測試繫統。通過建立數學模型,搭建試驗測量裝置,利用數據採集處理繫統得到瞭動態襬心漂移數據。該繫統採用高精度高頻響的激光位移傳感器保證瞭動態響應速度,程控調平機構解決瞭傳感器的精確定位問題,軟硬件濾波較好地剔除瞭擾動信號。繫統採樣頻率2 kHz,輸齣測量數據頻率不低于1 kHz;與靜態方法相比較,測量相對誤差不大于1%。結果錶明,該繫統能夠準確、實時地測試噴管全軸襬動時的襬心漂移軌跡。
위료개전유성분관전축파동동태파심측시,설계료일충이격광위이전감기、측공장치위기출적측시계통。통과건립수학모형,탑건시험측량장치,이용수거채집처리계통득도료동태파심표이수거。해계통채용고정도고빈향적격광위이전감기보증료동태향응속도,정공조평궤구해결료전감기적정학정위문제,연경건려파교호지척제료우동신호。계통채양빈솔2 kHz,수출측량수거빈솔불저우1 kHz;여정태방법상비교,측량상대오차불대우1%。결과표명,해계통능구준학、실시지측시분관전축파동시적파심표이궤적。
In order to investigate the dynamic test for pivot point of the omni-axial movable flexible joint nozzle,a test system basted on laser displacement sensor and measurement device was designed in this paper.By setting up mathematical model and con-structing a set of experimental system,the dynamic test data of pivot point was obtained by the data-acquisition system.The dynamic response speed of the test system was guaranteed by laser displacement sensor with high precision and high frequency.The problem of sensor accurate positioning was solved by the SPC leveling mechanism.Disturbance signals were eliminated by data processing.The sampling frequency and the output data frequency are respectively about 2 kHz and 1 kHz.Compared with static method,the relative error was not greater than 1%. Test result shows that the system can measure the track of pivot point reliably in real time when the flexible join nozzle is omni-axial moving.