! File: 2183C.PROP
! Database: PEPDB
! Date: 17-FEB-1994:02:45:33
coverpage:
title_1: MOVING TARGET TRACKING VERIFICATION TEST
proposal_for: OV/OLT
pi_fname: RODGER
pi_lname: DOXSEY
pi_inst: STSCI
pi_country: USA
pi_phone: 301-338-4750
hours_pri: 4.20
num_pri: 18
wf_pc: X
time_crit: X
! end of coverpage
abstract:
line_1: TEST OBJECTIVE:
line_2: Verify that the on-board parallax computation works properly for solar system
line_3: distance targets specified by a user supplied ephemeris. Verify that the
line_4: type-48 and type-51 commands executed by the on-board PGS software routines
line_5: work properly for tracking moving targets specified by a user supplied
line_6: ephemeris. Finally, verify that both the parallax and type-48 commands and the
line_7: parallax and type-51 commands work properly together.
!
! end of abstract
general_form_proposers:
lname: BROWN
fname: BOB
inst: ST SCI
country: USA
!
lname: NURRE
fname: JERRY
inst: MSFC
country: USA
!
lname: CALDWELL
fname: JOHN
inst: SUNY
country: USA
!
lname: DOXSEY
fname: RODGER
inst: ST SCI
country: USA
!
lname: STOCKMAN
fname: PETER
inst: ST SCI
country: USA
!
! end of general_form_proposers block
general_form_text:
question: 2
section: 1
line_1: The moving target tests proposed for this moving target tracking test verifies
line_2: the operation of the on-board moving target software through the use of user
line_3: supplied ephemerides against a static astrometric starfield (NGC188). The
line_4: first two test check out the parallax correction flight software. Two parallax
line_5: values are chosen, one at 0.5A.U. relative to the earth, the other at 1.0 A.U.
line_6: Each of three consecutive 10 minute PC exposures are actually composed of
line_7: alternating periods of the shutter being open (20 seconds) and closed (100
line_8: seconds). The PC CCDs are readout only after the last of the 5 shutter open
line_9: periods.
line_11: This method of PC exposure produces a sequence of 5 staggered streaks of the
line_12: star field. This data together with the PCS/FGS telemetry data is reduced to
line_13: check the validity of the parallax corrections. Short exposure guard frames
line_14: use a fixed target close to the endpoints of the user supplied ephemeris for
line_15: each test. These bracket the series of 10 minute exposures and provide the
line_16: basic reference data for the astrometric star field.
line_17: The third test uses a user supplied ephemeris that simulates a distant solar
line_18: system object with relatively simple non-linear motion against a static
line_19: astrometric star field. The SMS will require use of the type-48 command with
line_20: simplified secondary planetary motion coefficients to control the PCS. No
line_21: parallax corrections are performed. The exposures follow the same format as
line_22: described above for the parallax tests.
!
question: 2
section: 2
line_1: The fourth test uses a user supplied ephemeris that simulates a distant solar
line_2: system object with relatively simple linear motion against a static astrometric
line_3: star field. The SMS will require use of the type-51 command with profiled slew
line_4: rate and acceleration parameters to control the PCS. No parallax corrections
line_5: ar performed. The exposures follow the same format as described above for the
line_6: parallax tests.
line_8: The fifth test uses a user supplied ephemeris that simulates a solar system
line_9: object with a complex non-linear motion against a static astrometric star
line_10: field. Such an ephemeris, for example, might simulate a solar system satellite
line_11: undergoing maximum elongation as seen from the earth. The SMS will require use
line_12: of the type-48 command as in the third test and a parallax correction for 0.5
line_13: A.U. The exposures follow the same format as described above for the parallax
line_14: tests.
line_16: The sixth test uses a user supplied ephemeris that simulates a solar system
line_17: object with a complex linear motion against a static astrometric star field.
line_18: It is difficult to imagine a naturally occurring object that would undergo such
line_19: motion. However, this test will serve as an approximation to more complex
line_20: motion through the use of a piece-wise continuous ephemeris over very short
line_21: time periods. The SMS will require use of the type-51 command as in the fourth
line_22: test and a parallax correction of 0.5 A.U. The exposures follow the same
line_23: format as described above for the parallax tests.
!
question: 3
section: 1
line_1: Test Procedure:
line_2: ---------------
line_3: The general observing strategy is as follows:
line_5: 1) Take a short exposure with the WF/PC in PC mode.
line_7: 2) Start the ST moving (via one of the following: parallax, polynomials,
line_8: parallax and polynominals, profiled slew or parallax and profiled slew).
line_10: 3) Take three 10 minute PC exposures.
line_11: Use the Take Data Flag and the WF/PC Applications Processor (AP) to open
line_12: and close the shutter five times during each exposure. This will provide
line_13: reference times in the data headers and create gaps in the star trails
line_14: during the PC exposure. The star trails will be analyzed later to verify
line_15: proper tracking.
line_17: 4) Stop the ST motion.
line_19: 5) Take a second short PC exposure.
line_21: A more detailed test procedure follows:
!
question: 3
section: 2
line_1: * Configure the WF/PC *
line_3: 1) Configure the WF/PC to the Planetary Camera mode (PC - IMAGE)
line_4: 2) Select all 4 PC CCDs for the field of view (ALL)
line_5: 3) Select the V filter (F569W)
line_7: * Test 1 - Parallax Setting No. 1 *
line_9: 4) Start no gap sequence of activity
line_10: 5) Acquire Target Field No. 1
line_11: 6) Set parallax flag for no correction
line_12: 7) Take a 1 second PC guard frame exposure then readout (READ=YES)
line_13: 8) Set parallax for distance of 0.5A.U.
line_14: 9) Take 20 second PC exposure with no readout (READ=NO)
line_15: 10) Wait 100 seconds
line_16: 11) Repeat steps 9 and 10 three times
line_17: 12) Take 20 second PC exposure with readout (READ=OUT)
line_18: 13) Repeat steps 9 through 12 two times
line_19: 14) Repeat steps 6 and 7
line_20: 15) End no gap sequence of activity
!
question: 3
section: 3
line_1: * Test 2 - Parallax Setting No. 2 *
line_3: 16) Start no gap sequence of activity
line_4: 17) Acquire Target Field No. 2
line_5: 18) Repeat steps 6 and 7
line_6: 19) Set parallax for distance of 1.0A.U.
line_7: 20) Repeat steps 9 through 14
line_8: 21) End no gap sequence of activity
line_10: * Test 3 - Test of type-48 Command *
line_12: 22) Start no gap sequence of activity
line_13: 23) Acquire Target Field No. 3
line_14: 24) Repeat steps 6 and 7
line_15: 25) Turn off 38-type parallax correction flag
line_16: 26) Repeat steps 9 through 14 (use of tyep-48 commands with simplified
line_17: secondary planetary motion coefficients for simple motion)
line_18: 27) End no gap sequence of activity
!
question: 3
section: 4
line_1: * Test 4 - Test of type-51 Command *
line_3: 28) Start no gap sequence of activity
line_4: 29) Acquire Target Field No. 4
line_5: 30) Repeat steps 6 and 7
line_6: 31) Turn off 38-type parallax correction flag
line_7: 32) Repeat steps 9 through 14 (use of type-51 commands with profiled slew rate
line_8: and acceleration parameters for simple motion)
line_9: 33) End no gap sequence of activity
line_11: * Test 5 - Combine Parallax Test and use of Type-48 Command *
line_13: 34) Start no gap sequence of activity
line_14: 35) Acquire Target Field No. 5
line_15: 36) Repeat steps 6 and 7
line_16: 37) Set parallax for distance of 0.5A.U.
line_17: 38) Repeat steps 9 through 14 (use of type-48 commands with simplified
line_18: secondary planetary motion coefficients for complex motion)
line_19: 39) End no gap sequence of activity
!
question: 3
section: 5
line_1: * Test 6 - Combine Parallax Test and use of Type-51 Command *
line_3: 40) Start no gap sequence of activity
line_4: 41) Acquire Target Field No. 6
line_5: 42) Repeat steps 6 and 7
line_6: 43) Set parallax for distance of 0.5A.U.
line_7: 44) Repeat steps 9 through 14 (use of type-51 commands with profiled slew rate
line_8: and acceleration parameters for complex motion)
line_9: 45) End no gap sequence of activity
!
question: 4
section: 0
line_1: Submitted as an Observatory Level Test
!
question: 5
section: 0
line_1: Special scheduling request: Time-critical observations
line_3: Since all targets will be in the form of user supplied ephemerides, the
line_4: observations for this OLT will be time-critical.
line_6: Test Prerequisites:
line_8: - No observations performed during SAA passage
line_9: - Optical image quality should be near Level 1 (lambda/8)
line_10: - FGS/FGS OV alignments completed
line_11: - Acceptable errors of <= +/-0.5 arc seconds for OV phase
line_12: - WF/PC:
line_13: - Functional checkout
line_14: - Cooled to nominal operating temperature
line_15: - Preliminary focus setting established
line_16: - Geometrical tests completed (OV phase)
line_17: - Schedule this OLT during the early to mid OV mission phase
line_18: - Schedule test after the Raster/Dwell Scan Verification Test
line_19: - Mini-OFAD verification would be highly desireable but not necessary
line_20: - Require off-line access to the downlinked PCS/FGS engineering data
!
question: 7
section: 0
line_1: Real Time Data Analysis Requirements:
line_3: - Not anticipated at this time
line_5: Off Line Data Analysis Requirements:
line_7: - PASS FGS/SI attitude determination algorithms will be used to reduce
line_8: FGS star selector encoder readings to yield the spacecraft attitude
line_9: in approximately 5 second intervals throughout the observations.
!
question: 8
section: 0
line_1: All ephemerides used in this OLT will be supplied by the proposal team. Note
line_2: that the type-38 parallax correction flag is turned off during tests 3 and 4.
line_3: Distances specified for these tests must be very large. Also, the type of
line_4: command for PCS maneuvering (type-48 or -51) must accompany the appropriate
line_5: ephemeris so that the science scheduling team can flag the SMS accordingly.
!
question: 9
section: 0
line_1: Results of this OLT will be documented in an STScI Technical Report with
line_2: distribution to appropriate personnel. Portions of this test will be presented
line_3: at the HST symposium following the SV mission phase. Test results may also be
line_4: sumbitted for publication in an appropriate technical journal.
!
!end of general form text
general_form_address:
lname: DOXSEY
fname: RODGER
category: PI
inst: STSCI
addr_1: 3700 SAN MARTIN DRIVE
city: BALTIMORE
state: MD
zip: 21218
!
! end of general_form_address records
fixed_targets:
targnum: 1
name_1: NGC188-FIELD1A
descr_1: FIELD WITHIN NGC188
equinox: 1988
comment_1: TARGET POSITION CORRESPONDS TO
comment_2: FIRST POSITION OF USER SUPPLIED
comment_3: EPHEMERIS NO.1.
fluxnum_1: 1
fluxval_1: V=13 +/-1.0
!
targnum: 2
name_1: NGC188-FIELD1B
descr_1: FIELD WITHIN NGC188
equinox: ^
comment_1: TARGET POSITION CORRESPONDS TO
comment_2: FIRST POSITION OF USER SUPPLIED
comment_3: EPHEMERIS NO.1.
fluxval_1: ^
!
targnum: 3
name_1: NGC188-FIELD2A
descr_1: FIELD WITHIN NGC188
equinox: ^
comment_1: TARGET POSITION CORRESPONDS TO
comment_2: FIRST POSITION OF USER SUPPLIED
comment_3: EPHEMERIS NO. 2.
fluxval_1: ^
!
targnum: 4
name_1: NGC188-FIELD2B
descr_1: FIELD WITHIN NGC188
equinox: ^
comment_1: TARGET POSITION CORRESPONDS TO
comment_2: LAST POSITION OF USER SUPPLIED
comment_3: EPHEMERIS NO. 2.
fluxval_1: ^
!
targnum: 5
name_1: NGC188-FIELD3A
descr_1: FIELD WITHIN NGC188
equinox: ^
comment_1: TARGET POSITION CORRESPONDS TO
comment_2: FIRST POSITION OF USER SUPPLIED
comment_3: EPHEMERIS NO. 3.
fluxval_1: ^
!
targnum: 6
name_1: NGC188-FIELD3B
descr_1: FIELD WITHIN NGC188
equinox: ^
comment_1: TARGET POSITION CORRESPONDS TO
comment_2: LAST POSITION OF USER SUPPLIED
comment_3: EPHEMERIS NO. 3.
fluxval_1: ^
!
targnum: 7
name_1: NGC188-FIELD4A
descr_1: FIELD WITHIN NGC188
equinox: 1988
comment_1: TARGET POSITION CORRESPONDS TO
comment_2: FIRST POSITION OF USER SUPPLIED
comment_3: EPHEMERIS NO. 4.
fluxnum_1: 1
fluxval_1: V=13 +/- 1.0
!
targnum: 8
name_1: NGC188-FIELD4B
descr_1: FIELD WITHIN NGC188
equinox: ^
comment_1: TARGET POSITION CORRESPONDS TO
comment_2: LAST POSITION OF USER SUPPLIED
comment_3: EPHEMERIS NO. 4.
fluxval_1: ^
!
targnum: 9
name_1: NGC188-FIELD5A
descr_1: FIELD WITHIN NGC188
equinox: ^
comment_1: TARGET POSITION CORRESPONDS TO
comment_2: FIRST POSITION OF USER SUPPLIED
comment_3: EPHEMERIS NO. 5.
fluxval_1: ^
!
targnum: 10
name_1: NGC188-FIELD5B
descr_1: FIELD WITHIN NGC188
equinox: ^
comment_1: TARGET POSITION CORRESPONDS TO
comment_2: FIRST POSITION OF USER SUPPLIED
comment_3: EPHEMERIS NO. 5.
fluxval_1: ^
!
targnum: 11
name_1: NGC188-FIELD6A
descr_1: FIELD WITHIN NGC188
equinox: ^
comment_1: TARGET POSITION CORRESPONDS TO
comment_2: FIRST POSITION OF USER SUPPLIED
comment_3: EPHEMERIS NO. 6.
fluxval_1: ^
!
targnum: 12
name_1: NGC188-FIELD6B
descr_1: FIELD WITHIN NGC188
equinox: ^
comment_1: TARGET POSITION CORRESPONDS TO
comment_2: LAST POSITION OF USER SUPPLIED
comment_3: EPHEMERIS NO. 6.
fluxval_1: ^
!
! end of fixed targets
solar_system_targets:
targnum: 101
name_1: TEST-OBJ1
descr_1: SOLAR-SYSTEM TARGET-TEST OBJECT-1
lev1_1: POSITION DEFINED BY A USER
lev1_2: SUPPLIED EPHEMERIS FOR TEST
lev1_3: OBJECT-1 IN THE DIRECTION OF
lev1_4: CLUSTER NGC188.DISTANCE IS 0.5 AU
comment_1: TYPE-38 PARALLAX CORRECTION FLAG
comment_2: MUST BE ON FOR THIS TARGET.
fluxnum_1: 1
fluxval_1: V=13.0 +/- 1.0
!
targnum: 102
name_1: TEST-OBJ2
descr_1: SOLAR-SYSTEM TARGET-TEST OBJECT-2
lev1_1: POSITION DEFINED BY A USER
lev1_2: SUPPLIED EPHEMERIS FOR TEST
lev1_3: OBJECT-2 IN THE DIRECTION OF
lev1_4: CLUSTER NGC188.DISTANCE IS 1.0 AU
comment_1: TYPE-38 PARALLAX CORRECTION FLAG
comment_2: MUST BE ON FOR THIS TARGET.
fluxval_1: ^
!
targnum: 103
name_1: TEST-OBJ3
descr_1: SOLAR-SYSTEM TARGET-TEST OBJECT-3
lev1_1: POSITION DEFINED BY A USER
lev1_2: SUPPLIED EPHEMERIS FOR TEST
lev1_3: OBJECT-3 IN THE DIRECTION OF
lev1_4: CLUST.NGC188.DISTANCE VERY LARGE.
comment_1: TYPE-38 PARALLAX CORRECTION FLAG
comment_2: MUST BE OFF FOR THIS TARGET.
comment_3: USE TYPE-48 COMMAND FOR PCS
comment_4: MANEUVERING.
fluxval_1: ^
!
targnum: 104
name_1: TEST-OBJ4
descr_1: SOLAR-SYSTEM TARGET-TEST OBJECT-4
lev1_1: POSITION DEFINED BY A USER
lev1_2: SUPPLIED EPHEMERIS FOR TEST
lev1_3: OBJECT-4 IN THE DIRECTION OF
lev1_4: CLUST.NGC188.DISTANCE VERY LARGE.
comment_1: TYPE-38 PARALLAX CORRECTION FLAG
comment_2: MUST BE OFF FOR THIS TARGET.
comment_3: USE TYPE-51 COMMAND FOR PCS
comment_4: MANEUVERING.
fluxnum_1: 1
fluxval_1: V = 13.0 +/- 1.0
!
targnum: 105
name_1: TEST-OBJ5
descr_1: SOLAR-SYSTEM TARGET-TEST OBJECT-5
lev1_1: POSITION DEFINED BY A USER
lev1_2: SUPPLIED EPHEMERIS FOR TEST
lev1_3: OBJECT-5 IN THE DIRECTION OF
lev1_4: CLUST.NGC188.DISTANCE IS 0.5 AU.
comment_1: TYPE-38 PARALLAX CORRECTION FLAG
comment_2: MUST BE ON FOR THIS TARGET.
comment_3: USE TYPE-48 COMMAND FOR PCS
comment_4: MANEUVERING.
fluxnum_1: 1
fluxval_1: V=13.0 +/-1.0
!
targnum: 106
name_1: TEST-OBJ6
descr_1: SOLAR-SYSTEM TARGET-TEST OBJECT-6
lev1_1: POSITION DEFINED BY A USER
lev1_2: SUPPLIED EPHEMERIS FOR TEST
lev1_3: OBJECT-6 IN THE DIRECTION OF
lev1_4: CLUST.NGC188.DISTANCE IS 0.5 AU.
comment_1: TYPE-38 PARALLAX CORRECTION FLAG
comment_2: MUST BE ON FOR THIS TARGET.
comment_3: USE TYPE-51 COMMAND FOR PCS
comment_4: MANEUVERING.
fluxval_1: ^
!
! end of solar system targets
! No generic target records found
exposure_logsheet:
linenum: 1.000
sequence_1: DEFINE
sequence_2: GUARD
targname: #
config: PC
opmode: IMAGE
aperture: ALL
sp_element: F569W
num_exp: 1
time_per_exp: 1S
fluxnum_1: 1
priority: 1
comment_1: GUARD FRAME EXPOSURE.
!
linenum: 5.000
sequence_1: DEFINE
sequence_2: NORMAL
targname: #
config: PC
opmode: IMAGE
aperture: ALL
sp_element: F569W
num_exp: 1
time_per_exp: 20S
fluxnum_1: 1
priority: 1
param_1: READ=NO
req_1: SEQ 5-9 NO GAP
comment_1: 1 OF 5 PC STAR TRAIL EXPOSURES.
!
linenum: 6.000
sequence_1: ^
targname: ^
config: ^
opmode: ^
aperture: ^
sp_element: ^
num_exp: ^
time_per_exp: ^
fluxnum_1: ^
priority: ^
param_1: ^
req_1: AFTER 5 BY 120S +/- 1S
comment_1: 2 OF 5 PC STAR TRAIL EXPOSURES.
!
linenum: 7.000
sequence_1: ^
targname: ^
config: ^
opmode: ^
aperture: ^
sp_element: ^
num_exp: ^
time_per_exp: ^
fluxnum_1: ^
priority: ^
param_1: ^
req_1: AFTER 6 BY 120S +/- 1S
comment_1: 3 OF 5 PC STAR TRAIL EXPOSURES.
!
linenum: 8.000
sequence_1: ^
targname: ^
config: ^
opmode: ^
aperture: ^
sp_element: ^
num_exp: ^
time_per_exp: ^
fluxnum_1: ^
priority: ^
param_1: ^
req_1: AFTER 7 BY 120S +/-1S
comment_1: 4 OF 5 PC STAR TRAIL EXPOSURES.
!
linenum: 9.000
sequence_1: ^
targname: ^
config: ^
opmode: ^
aperture: ^
sp_element: ^
num_exp: ^
time_per_exp: ^
fluxnum_1: ^
priority: ^
param_1: READ=YES
req_1: AFTER 8 BY 120S +/-1S
comment_1: 5 OF 5 PC STAR TRAIL EXPOSURES.
!
linenum: 30.000
sequence_1: USE
sequence_2: GUARD
targname: NGC188-FIELD1A
req_1: SEQ 30-34 NO GAP;
req_2: AT TBD-PII
!
linenum: 31.000
sequence_1: USE
sequence_2: NORMAL
targname: TEST-OBJ1
comment_1: PARALLAX SET TO 0.5 A.U.
!
linenum: 32.000
sequence_1: USE
sequence_2: NORMAL
targname: ^
comment_1: PARALLAX SET TO 0.5 A.U.
!
linenum: 33.000
sequence_1: USE
sequence_2: NORMAL
targname: ^
comment_1: PARALLAX SET TO 0.5 A.U.
!
linenum: 34.000
sequence_1: USE
sequence_2: GUARD
targname: NGC188-FIELD1B
!
linenum: 40.000
sequence_1: USE
sequence_2: GUARD
targname: NGC188-FIELD2A
req_1: SEQ 40-44 NO GAP;
req_2: AT TBD-PII
!
linenum: 41.000
sequence_1: USE
sequence_2: NORMAL
targname: TEST-OBJ2
comment_1: PARALLAX SET TO 1.0 A.U.
!
linenum: 42.000
sequence_1: USE
sequence_2: NORMAL
targname: ^
comment_1: PARALLAX SET TO 1.0 A.U.
!
linenum: 43.000
sequence_1: USE
sequence_2: NORMAL
targname: ^
comment_1: PARALLAX SET TO 1.0 A.U.
!
linenum: 44.000
sequence_1: USE
sequence_2: GUARD
targname: NGC188-FIELD2B
!
linenum: 50.000
sequence_1: USE
sequence_2: GUARD
targname: NGC188-FIELD3A
req_1: SEQ 50-54 NO GAP;
req_2: AT TBD-PII
!
linenum: 51.000
sequence_1: USE
sequence_2: NORMAL
targname: TEST-OBJ3
comment_1: SIMPLE NON-LINEAR MOTION WITH
comment_2: DISTANCE SET TO INFINITY.
!
linenum: 52.000
sequence_1: USE
sequence_2: NORMAL
targname: ^
comment_1: SIMPLE NON-LINEAR MOTION WITH
comment_2: DISTANCE SET TO INFINITY.
!
linenum: 53.000
sequence_1: USE
sequence_2: NORMAL
targname: ^
comment_1: SIMPLE NON-LINEAR MOTION WITH
comment_2: DISTANCE SET TO INIFINITY.
!
linenum: 54.000
sequence_1: USE
sequence_2: GUARD
targname: NGC188-FIELD3B
!
linenum: 60.000
sequence_1: USE
sequence_2: GUARD
targname: NGC188-FIELD4A
req_1: SEQ 60-64 NO GAP;
req_2: AT TBD-PII
!
linenum: 61.000
sequence_1: USE
sequence_2: NORMAL
targname: TEST-OBJ4
comment_1: SIMPLE LINEAR MOTION WITH DISTANCE
comment_2: SET TO INFINITY.
!
linenum: 62.000
sequence_1: USE
sequence_2: NORMAL
targname: ^
comment_1: SIMPLE LINEAR MOTION WITH DISTANCE
comment_2: SET TO INFINITY.
!
linenum: 63.000
sequence_1: USE
sequence_2: NORMAL
targname: ^
comment_1: SIMPLE LINEAR MOTION WITH DISTANCE
comment_2: SET TO INFINITY.
!
linenum: 64.000
sequence_1: USE
sequence_2: GUARD
targname: NGC188-FIELD4B
!
linenum: 70.000
sequence_1: USE
sequence_2: GUARD
targname: NGC188-FIELD5A
req_1: SEQ 70-74 NO GAP;
req_2: AT TBD-PII
!
linenum: 71.000
sequence_1: USE
sequence_2: NORMAL
targname: TEST-OBJ5
comment_1: COMPLEX NON-LINEAR MOTION WITH
comment_2: DISTANCE SET TO 0.5 A.U.
!
linenum: 72.000
sequence_1: USE
sequence_2: NORMAL
targname: ^
comment_1: COMPLEX NON-LINEAR MOTION WITH
comment_2: DISTANCE SET TO 0.5 A.U.
!
linenum: 73.000
sequence_1: USE
sequence_2: NORMAL
targname: ^
comment_1: COMPLEX NON-LINEAR MOTION WITH
comment_2: DISTANCE SET TO 0.5 A.U.
!
linenum: 74.000
sequence_1: USE
sequence_2: GUARD
targname: NGC188-FIELD5B
!
linenum: 80.000
sequence_1: USE
sequence_2: GUARD
targname: NGC188-FIELD6A
req_1: SEQ 80-84 NO GAP;
req_2: AT TBD-PII
!
linenum: 81.000
sequence_1: USE
sequence_2: NORMAL
targname: TEST-OBJ6
comment_1: COMPLEX LINEAR MOTION WITH DISTANCE
comment_2: SET TO 0.5 A.U.
!
linenum: 82.000
sequence_1: USE
sequence_2: NORMAL
targname: ^
comment_1: COMPLEX LINEAR MOTION WITH DISTANCE
comment_2: SET TO 0.5 A.U.
!
linenum: 83.000
sequence_1: USE
sequence_2: NORMAL
targname: ^
comment_1: COMPLEX LINEAR MOTION WITH DISTANCE
comment_2: SET TO 0.5 A.U.
!
linenum: 84.000
sequence_1: USE
sequence_2: GUARD
targname: NGC188-FIELD6B
!
! end of exposure logsheet
! No scan data records found