支撑压力起飞MA1:=MA(CLOSE,...

支撑压力起飞
MA1:=MA(CLOSE,5);
压力:=MA(REF(HHV(C,30),1),2);
支撑:=MA(REF(LLV(C,30),1),2);
SH:UPNDAY(压力,1) AND UPNDAY(支撑,1) AND UPNDAY(MA1,5);