Last updated: 6 Sep 1997, 13:45 PDT, Data Controller: Allen R. Sirota
Sequence 56020C:
Proceed with Nominal Execution
Operational Constraints (for Sol 64 Sequence):
Operational Constraints (General):
SEQUENCE EXECUTION STATUS (EOD Sol 63):
VEHICLE STATE:
(AS OF COMMAND: 12136, Level 3 Health Check
BATTERY STATE/USAGE(AS OF EOD SOL 63)
THEY'RE DEAD, JIM
SUBSYSTEM STATUS (AS OF EOD SOL 63):
NAVIGATION PERFORMANCE:
THERMAL PERFORMANCE:
TELECOM PERFORMANCE
MOBILITY PERFORMANCE:
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.
SUMMARY REPORT
RETRANSMIT REQUESTS
SEQUENCE PLANNING RECOMMENDATIONS
Engineering Requests:
SEQUENCE EXECUTION STATUS & VEHICLE STATE
Execution: Nominal
State: Running
Wakeup: SCET 9/6/97 14:49, Sol 63 7:54 MLST
Crit Errors: None
Executing sequence 56020C
SCET: 9/6/97 19:02, MLST: Sol 63 12:00
)
Mission Phase: Primary
Mode: Executing
Config: Moderate roll and pitch
APXS Deployed onto Half Dome
Power: No Battery Mission
Device Status: Gyro force failed
Z accel force failed
RFW temp. force failed
Batteries Force Failed
Temp (Internal): Nominal
Temp (External): Nominal
Temp:(Modem): Nominal
Parameter Initial Final IMP EOD Parameter Initial Final
---------------------------------------------------------------------------------
X Position (m) -4.942 -4.942 ? LBogie (deg) +16.96 +16.88
Y Position (m) -3.876 -3.876 ? Rbogie (deg) -16.16 -16.16
Heading (deg) +89.1 +89.1 ? Diff (deg) +13.44 +13.44
Pitch (deg) +15.5 +15.5 (+ Pitch -> Front down)
Roll (deg) +16.7 +16.7 (+ Roll -> Roll to Starboard)
ADM Pos (deg) -99.84 -99.84 (deployed)
LFS (deg) +1.9 +1.9 RFS (deg) -1.3 -1.3
LRS (deg) 0.0 0.0 RRS (deg) -1.3 -1.3
--------------------------------------------------------------------------------
ADM Bumper Solar
UL UR B RB LB LR RR RF LF
Mask 1 1 1 1 1 1 1 1 1
State 0 1 1 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
S/S Status Comments
C&N Nominal None
MTM Nominal None
Thermal Nominal None
Power Nominal Batteries Depleted, MAE reading low
Telecom Nominal None
TRAVERSE HAZARDS (DETECTED)
None
TELEMETRY VOLUME
DATA VOLUME SUMMARY (BY APID)*
APID #PKTS #BYTES #Mbits
----------------------------------
4 14 4107 0.03286
5 71 3315 0.02652
6 1 60 0.00048
7 9 504 0.00403
8 0 0 0.00000
9 0 0 0.00000
10 0 0 0.00000
12 8 8560 0.06848
23 0 0 0.00000
24 0 0 0.00000
25 0 0 0.00000
29 0 0 0.00000
----------------------------------
103 16546 0.13237
*All data downlinked on this Sol INCLUDING retransmitted data.
SUBSYSTEM REPORTS
Report Pending
Report Pending
Telecom system performance was nominal this sol and link performance is consistent with te temperature and data volume.
There are no telecom operational constraints for future rover operations.
The end-of-sol communication system performance for the downlink was as follows:
SOL 63 DOWNLINK TELECOM STATISTICS
Rov Radio Temp Low = -23.1
Rov Radio Temp High = 32.6
Rov Radio Temp Avg = 20.5
LMRE Radio Temp Low = -9.7
LMRE Radio Temp High = 19.6
LMRE Radio Temp Avg = 9.5
Rx Current Low = 43.5
Rx Current High = 49.3
Rx Current Avg = 47.2
Tx Current Low = 159.5
Tx Current High = 159.5
Tx Current Avg = 159.5
LMRE Good Frames = 255
LMRE Garbled Frames = 146
Avg LMRE Link Quality%= 63.6
TX_CH_FRAMES = 761
RX_CH_FRAMES = 318
Total Frame Resends = 443
Avg Rover Link Quality%= 41.8
COM:Bad CRC Errors = 18
COM:Timeout Errors = 51463
COM:Rx Abort Errors = 736
COM:No Sync Errors = 4
COM:RX Com Errors = 38026
In planning the sequence for Sol 64 and beyond, the revised modem heating strategy used shuld be followed:
For rover wakeups on solar power, modem heating is only needed if communications is needed in the morning. In this situation set modem heating
to 0 and reheat to 300 seconds. Also, if there are afternoon only downlink sessions, then no modem heating is required after wakeup on solar.
The rover modem should be commanded in the next-day runout sequence to perform a 300 second modem reheat at wakeup. Later in the day, 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. However, if the LMRE radio is off, then the reheat to get to +30C is not needed. This requires some coordination of
timing between the LMRE ON times and the rover transmissions. The sequence planners should consider the uncertainty in event completion times
introduced by any required modem reheating cycles.
Report pending
Report pending
TELEMETRY PROCESSING ANOMALIES
None
PRESS RELEASE