传感技术学报
傳感技術學報
전감기술학보
Journal of Transduction Technology
2013年
8期
1168-1172
,共5页
李建宇%张朝杰%金小军%娄延年
李建宇%張朝傑%金小軍%婁延年
리건우%장조걸%금소군%루연년
测控应答机%直接上变频%镜像频率%发射机
測控應答機%直接上變頻%鏡像頻率%髮射機
측공응답궤%직접상변빈%경상빈솔%발사궤
transponder%direct-up conversion%image frequency%transmitter
设计并实现了一种新型适用于微小卫星的小型化、低功耗S波段发射机结构。该结构利用了DAC输出的镜像信号,用较低的处理速率产生比采样时钟频率更高的中频信号,实现一次混频将下行信号搬移到发射频率上,有效地减小了发射机的面积及功耗。发射机在一块印制电路板上实现,实际测试功耗约为2.2W,发射功率为26dBm,可满足轨道高度小于1000km的低轨微小卫星的测控需求。
設計併實現瞭一種新型適用于微小衛星的小型化、低功耗S波段髮射機結構。該結構利用瞭DAC輸齣的鏡像信號,用較低的處理速率產生比採樣時鐘頻率更高的中頻信號,實現一次混頻將下行信號搬移到髮射頻率上,有效地減小瞭髮射機的麵積及功耗。髮射機在一塊印製電路闆上實現,實際測試功耗約為2.2W,髮射功率為26dBm,可滿足軌道高度小于1000km的低軌微小衛星的測控需求。
설계병실현료일충신형괄용우미소위성적소형화、저공모S파단발사궤결구。해결구이용료DAC수출적경상신호,용교저적처리속솔산생비채양시종빈솔경고적중빈신호,실현일차혼빈장하행신호반이도발사빈솔상,유효지감소료발사궤적면적급공모。발사궤재일괴인제전로판상실현,실제측시공모약위2.2W,발사공솔위26dBm,가만족궤도고도소우1000km적저궤미소위성적측공수구。
A new S-band transmitter structure with small volume and low-power consumption is presented for LEO micro-satellite applications. Due to the use of the image frequency of the DAC,the IF signal of higher frequency is generated with a relatively low processing rate. In this way, the downlink signal is moved to the transmitting frequency with one mixing stage, thus effectively reducing the transmitter's volume and power consumption. The transmitter was implemented on a printed circuit board,and the test results showed that a transmit power of 26 dBm and a power consumption of only 2. 2 W are achieved. The transmitter can be used in micro-satellites in orbits lower than 1 000 km.