Last updated: 31 July 1997, 17:00 PST, Data Controller: Allen R. Sirota
Summary Report |
|
Retransmit Status:
SEQUENCE EXECUTION STATUS:
Execution: | Nominal |
State: | Idle |
Wakeup: | Solar, 1997 212 SOL 25 07:32 LTST |
Crit Errors: | None |
Executing sequence 52710D |
VEHICLE STATE: (AS OF COMMAND: 27113, Commanded Health Check SCET: 7/31/97 21:24:56 )
Mission Phase: | Primary |
Mode: | Executing |
Config: | Nominal |
At edge of mermaid dune | |
Power: | Nominal |
Device Status: | Z Accelerometer Forced bad |
RFW Temp. sensor Forced Bad | |
LF Wheel Motor unjammed | |
Temp (Internal): | Nominal |
Temp (External): | Nominal |
Temp:(Modem): | Nominal |
Parameter Initial Final Imp EOD Parameter Initial Final
---------------------------------------------------------------------------------
X Position ( -2.349 -5.256 ? LBogey (deg) -2.72 -3.60
Y Position (m) +3.938 +2.907 ? RBogey (deg) -8.48 -0.80
Heading (deg) +214.7 +16.6 ? Diff (deg) -3.68 -3.36
Pitch (deg) +1.2 +1.2 (+ Pitch -> Front down)
Roll (deg) -5.9 +2.4 (+ Roll -> Roll to Starboard)
ADM Pos (deg) -1.28 -1.28 (Fully Retracted)
LFS (deg) -9.6 0.0 RFS (deg) -16.6 -1.3
LRS (deg) +11.5 0.0 RRS (deg) +15.4 -1.9
--------------------------------------------------------------------------------
BATTERY STATE/USAGE**
Total Battery Remaining (Amp*hrs)
Category Allocation Initial Final *Predicted
--------------------------------------------------------------
Operations 10 4.437*** 4.388 4.288
Science 10 5.620 5.620 5.620
Technology 10 7.534 7.534 7.534
--------------------------------------------------------------
Total 30 17.591 17.542 17.442
*** This is believed to be lower than real by about 0.4 Ahrs
due to some change in the battery state of charge registers.
** reflects transfer of two hours from technology to science
* at completion of sequence 52610B.
ADM | Bumper | Solar | |||||||
---|---|---|---|---|---|---|---|---|---|
UL | UR | B | RB | LB | LR | RR | RF | LF | |
Mask | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 |
State | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
ERROR FLAGS | |||||||||
---|---|---|---|---|---|---|---|---|---|
Skip | GenFail | InvalidCmd | WEB_Hot | NoPwr | NonTrav | DevNA | DevFail | Timeout | |
Mask | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 |
State | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
SUBSYSTEM STATUS:
S/S | Status | Comments |
---|---|---|
C&N | Nominal | None |
MTM | Nominal | RF Wheel Temp Sensor H/W failure |
Thermal | Nominal | None |
Power | Nominal | None |
Telecom | Nominal | None |
*All data downlinked on this Sol INCLUDING retransmitted data.
NAVIGATION PERFORMANCE:
The rover is heading to Mermaid Dune, tries to finish up what have left
off in yesterday traversal.
CONSTRAINTS:
THERMAL PERFORMANCE:
Recommendations:
TELECOM PERFORMANCE
STATISTICS
RECOMMENDATIONS
MOBILITY PERFORMANCE:
Recommendations:
POWER PERFORMANCE:
TBD
Web Page Authors: Henry W. Stone and
Allen.R.Sirota All information on this site, including text and images describing the
Rover is copyright © 1997, Jet Propulsion Laboratory, California Institute of Technology and the National Aeronautics and Space Administration.
TRAVERSE HAZARDS (DETECTED)
27050 turn_to (-2199, 4419) 930C: AZ1
27057 move (-2632, 4121) 97B3: AX2 AZ1
27057 move (-2704, 4072) 983C: AZ1
27062 goto (-3116, 3779) A49C: AZ1
27062 goto (-3283, 3526) A8B3: AZ1
27062 goto (-3324, 3464) A960: AZ1
27062 goto (-3409, 3332) A9A1: AZ1
27062 goto (-3563, 3095) A8AC: AZ1
27062 goto (-3588, 3057) A979: AZ1
27062 goto (-3718, 2844) A981: AZ1
27062 goto (-3863, 2616) A82B: AZ1
27062 goto (-3980, 2439) A91E: AZ1
27064 turn_at (-4063, 2289) 713C: AZ1
27068 goto (-4052, 2281) 6BF7: AZ1
27068 goto (-5127, 2822) 6AA2: AY0
27068 goto (-5143, 2831) 6A4C: AZ1
27068 goto (-5190, 2862) 6827: AZ1
27068 goto (-5243, 2897) 678C: AY1 AZ2
27070 turn_to (-5256, 2907) 1D25: AZ2
TELEMETRY VOLUME
DATA VOLUME SUMMARY (BY APID)*
APID #PKTS #BYTES #Mbits
----------------------------------
4 30 8817 0.07054
5 88 10906 0.08725
6 2 120 0.00096
7 1 40 0.00032
8 102 188348 1.50678
9 0 0 0.00000
10 0 0 0.00000
12 0 0 0.00000
23 0 0 0.00000
24 0 0 0.00000
25 423 828292 6.62634
29 15 18010 0.14408
----------------------------------
661 1054533 8.43626
SUBSYSTEM REPORTS
ACTIVITIES:
Perform wakeup every 2 hours for overnight thermal data on Sol 27
evening/Sol 28 morning. Tests 9.1 and 9.9 will be requested for Sol 28 morning
Telecom system performance was particularly good this sol, and the revised rover mdem heating strategy
recommended for this sol was effective. A review of the data plots for this sol aain shows correlation
between good rover-to-lander communication throughput and rover modem temperaturesabove roughly
+30 C. There are indications that three, and perhaps four, modem reheating cycleswere initiated
automatically by the rover after experiencing excessive retries on the rover-to-lader link.
Rov Radio Temp Low = -18.6
Rov Radio Temp High = 33.3
Rov Radio Temp Avg = 15.1
LMRE Radio Temp Low = 2.0
LMRE Radio Temp High = 21.8
LMRE Radio Temp Avg = 15.7
Rx Current Low = 43.5
Rx Current High = 49.3
Rx Current Avg = 46.0
Tx Current Low = 142.1
Tx Current High = 162.4
Tx Current Avg = 151.8
LMRE Good Frames = 3088
LMRE Garbled Frames = 2413
Avg LMRE Link Quality%= 56.1
TX_CH_FRAMES = 6396
RX_CH_FRAMES = 6385
Total Frame Resends = 11
Avg Rover Link Quality%= 99.8
COM:Bad CRC Errors = 8
COM:Timeout Errors = 16556
COM:Rx Abort Errors = 615
COM:No Sync Errors = 0
COM:RX Com Errors = 27194
In planning the sequence for Sol 28 and beyond, the revised modem heating strategyfirst used today (Sol
27) should be followed:
The rover modem should be commanded in the next-day runout sequence to perform a 600 second modem
heating at wakeup. If no overnight APXS operations are to be conducted, the wakeup rover modem
heating should be extended to 900 seconds. Modem reheating should be triggered by an excessive number
of frame retries on the rover-to-lander link, and the reheating should continue for five minutes or until the
rover modem reaches +30 C. The sequence planners should consider the uncertainty in event completion
times introduced by any required modem reheating cycles.
We are continuing our suspension of the previous recommendation to operate on LMRE-A for ten minutes
prior to the expected rover wakeup time.
Based upon the data returned in the health checks returned in SOL 27,
the Power Subsystem is in good health with no operational problems noted.
The output of the short circuit current cell in the MAE is used with the MAE
temperature measurment to predict the solar panel power available to the rover
at that time. By comparing this derived channel for the same time for
sequential days one should be able to determine any changes in the capability
of the solar panel. There are some factors that make it impossible to do a
quantitative assessment of the solar panel such as the change of tilt from day
to day and the fact that we don't have data for the same time each day.
However the general trend of the available power can be seen and for the rover
on Mars, it is decreasing. This is in spite of the fact that Mars continues to
decrease its distance from the sun. The decrease in solar panel power availableis,
however in agreement with the data taken by the MAE dust experiment.
TELEMETRY PROCESSING ANOMALIES
PRESS RELEASE