Mro On Approach, TCM-3 not required |
Mro On Approach, TCM-3 not required |
Feb 3 2006, 11:06 PM
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#1
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Member Group: Members Posts: 134 Joined: 13-March 05 Member No.: 191 |
MRO has shifted from the cruise phase to Approach phase. Apparently, the trajectory is so good that TCM-3 was cancelled. This is good news for the prospects for a long life for MRO supporting future missions. TCM-4 is on Feb 28, and MOI on March 10. Only 5 weeks away!
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Mar 10 2006, 08:02 AM
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#2
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Member Group: Members Posts: 370 Joined: 12-September 05 From: France Member No.: 495 |
Watch Mars Reconnaissance Orbiter's Doppler Plot in real time during MOI !
http://marsprogram.jpl.nasa.gov/mro/mission/tl_doppler.html Mars Orbit Insertion - Sequence of Events http://marsprogram.jpl.nasa.gov/mro/mission/tl_moi-soe.html |
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Mar 10 2006, 03:14 PM
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#3
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Member Group: Members Posts: 624 Joined: 10-August 05 Member No.: 460 |
Watch Mars Reconnaissance Orbiter's Doppler Plot in real time during MOI ! http://marsprogram.jpl.nasa.gov/mro/mission/tl_doppler.html Mars Orbit Insertion - Sequence of Events http://marsprogram.jpl.nasa.gov/mro/mission/tl_moi-soe.html Utterly cool. We are seeing a sawtooth in the residuals @ ~6 minute intervals - is this due to attitude control, solution harmonics or what? |
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Mar 10 2006, 05:01 PM
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#4
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Senior Member Group: Members Posts: 1465 Joined: 9-February 04 From: Columbus OH USA Member No.: 13 |
Utterly cool. We are seeing a sawtooth in the residuals @ ~6 minute intervals - is this due to attitude control, solution harmonics or what? Interesting item from 2001 Mars Odyssey orbit determination during interplanetary cruise: The resolution of the graph makes it hard to read, but it look like the amplitude of the sawtooth is a bit larger than with MRO (~5x), and the period about 15 minutes. QUOTE During the TCM-2 data arc, a couple passes of Doppler
residuals such as that shown in Figure 5 exhibited a peculiar sawtooth pattem. Because it appeared that we were having problems fitting the data without the gasleak acceleration estimation, we became concerned that this may have been more evidence of serious problems in the SIC modeling, the SDST, DSN hardware or the ODP. Several DSN and NAG experts helped analyze these unusual patterns, but no definitive explanation was found. The DSN tracking procedures for Odyssey had been to follow the S/C’s downlink frequency within a fairly tight bandwidth by periodically ramping the uplink signal. It was believed that this ramping of the signal could have contributed to this problem, especially if the values of the ramp rates were being truncated, but no evidence of this was found. In the case that this data was incorrect, our procedures were to remove the data, however, it was determined that the data had little effect on the OD solutions, especially due to the signatures’ high fi-equency nature. -------------------- |
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Mar 10 2006, 05:40 PM
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#5
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Member Group: Members Posts: 624 Joined: 10-August 05 Member No.: 460 |
Interesting item from 2001 Mars Odyssey orbit determination during interplanetary cruise: The resolution of the graph makes it hard to read, but it look like the amplitude of the sawtooth is a bit larger than with MRO (~5x), and the period about 15 minutes. Thanks - this is a good read, and the unmodel aspect - small forces corrections - required to hit the target make the cancelation of the finally 3-4 corrections very impressive navigation! Oh, and the saw tooth? Still an unsolved mystery:) |
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