PROC V_FL_SUN_TST
;Version 5 	
GOTO BEGIN
;
;#**************************************************************************
;#	****PROCEDURE HEADER****
;#
;# 	1.0 	Introduction
;#
;#		1.1	FOT Name:  V_FL_SUN_TST	   
;#		   	VIRGO Name:  Sun Test Mode (PROC 20)  	 
;#		   	Issue/Rev:  2.8   	
;#			Simulator Validation Status:
;#
;#		1.2	Date Created:  08-AUG-95 
;#			    Revision:  1. 31-AUG-95	HB
;#						2. 26-OCT-95	HB
;#						3. 16-JAN-96	HB
;#						4. 16-JAN-96	TB
;#						5. 23-MAR-96	HB
;#
;#		1.3	Change Description:	
;#
;#			1. Made flight ready.  Changed name from v_ts_sun_tst.  Added
;#			   two WAIT statements in the SPM test segment.  Added WAIT
;#			   statement in the DIARAD test segment.  Changed TM checks to
;#			   eliminate hard WAITs.
;#			2. Changed data word for PMO-A cover open from 800B to 800C.
;#			   Changed data word for first command in radiometers to nominal
;#			   mode, DIARAD Left, PMO-A from 909F to 90BF.
;#			3. Major changes.  Most commands deleted. 
;#			4. Deleted /VZML,800B 
;#			5. Deleted /VZML,800E.  Replaced VZML,400C with VZML,4008.
;#			   Replaced VZML,300C with VZML,3008.
;#
;#		1.4	Point of Contact:  CCazeau	
;#			FOT Author:  HBenefield  	ATSC/SOHO	286-4799
;#
;#**************************************************************************
;#	2.0	Description
;#
;#		2.1	Narrative Description
;#
;#			Procedure to start a first sun test mode after test/warm-up
;#			mode initialized at day 5.
;#
;#		2.2	Intended Use:
;#			
;#			Planned to be used at Day 23.
;#		
;#		2.3	Duration:	170 minutes
;#
;#		2.4	References:
;#			PAGES:  V_STATUS, V_TEMP_STAT, V_VOLT_HKCAL, I_EXP_STAT
;#
;#**************************************************************************
;#	3.0	Instructions for Use:
;#
;#		3.1	Parameters Required
;#
;#			None.
;#
;#		3.2	Critical Activities
;#
;#			None.
;#
;#		3.3	Special Constraints or Activities
;#
;#			The VIRGO commands execute on a 3 minute cycle.  Only one
;#			command can be sent between command executions.
;#     		
;#**************************************************************************
;#	4.0	STEPS:

BEGIN:

LOCAL EKS, WHY

IF (P@CMD_STATE#TELECOMMAND = "AVAILABLE") THEN
ELSE
	/CLEAR		;Clearing the Command Buffer.
ENDIF

;#**************************************************************************
;#	Start PMO Test
;#**************************************************************************

/VZML,909E	;Ref1, SPM-B, PMO-B, BU:  PMO-A Current.
WAIT			;Verify contents of command buffer.
/SEND

WAIT UNTIL(VSTCRETN=H'909E')		;Check TC return.

LET EKS = VS1PMB MOD 8
LET WHY = (VS1PMB - EKS)/8

WAIT UNTIL (WHY = 1)	;Check PMO6-B status (VS1PMB=B'1XXX')

/VZML,4008	;PMO-B:  LU en, Shutter Auto.
WAIT			;Verify contents of command buffer.
/SEND

WAIT UNTIL(VSTCRETN=H'4008')		;Check TC return.

/VZML,3008	;PMO-A:  LU en, Shutter Auto.
WAIT			;Verify contents of command buffer.
/SEND

WAIT UNTIL(VSTCRETN=H'3008')		;Check TC return.

/VZML,800C	;Cover open PMO-A.
WAIT			;Verify contents of command buffer.
/SEND

WAIT UNTIL(VSTCRETN=H'800C')		;Check TC return.

WAIT	;Verify science data for sun

/VZML,800D	;Cover open PMO-B.
WAIT			;Verify contents of command buffer.
/SEND

WAIT UNTIL(VSTCRETN=H'800D')		;Check TC return.

WAIT	;Verify science data for sun

;#**************************************************************************
;#	Start SPM Test
;#**************************************************************************

/VZML,800A	;Cover open SPM-A.
WAIT			;Verify contents of command buffer.
/SEND

WAIT UNTIL(VSTCRETN=H'800A')		;Check TC return.


;#************************************************************************** 
;#	5.0	Final Constraints
;#
;#		None.
;#
;#**************************************************************************
ENDPROC