
General
TDRSS tracking support provides all position, time, and frequency data necessary
to maintain precise customer spacecraft orbit prediction (acquisition), orbit
determination (tracking), and attitude determination and control.
This portion of the knowledge base includes the following additional TDRSS
tracking information:
Overview
of the TDRSS Acquisition/Tracking Support Cycle
Nominal
Tracking
Cross
- Support Tracking
Tracking
Accuracy
Attitude
and Control Support
Tracking
of the TDRSs
Tracking
Data Computed at the Customer Flight Platform (TONS)
The TDRSS acquisition/tracking support cycle may be summarized as the following:
- The GSFC Flight Dynamics Facility
(FDF) can provide customers with orbit planning and accuracy studies
during the mission planning phase.
- During customer S/C operations, the White Sands Complex(WSC) extracts
tracking data (range and range rate data ) from the customer's downlinked
telemetry link to TDRSS.
- WSC sends, via NISN, tracking data in TDRSS Tracking
Data Format to GSFC's Flight Dynamics Facility (FDF)
- The FDF places this data into temporary storage and periodically makes
ephemeris (the set of position and velocity vectors ) out of the buffered
data. After computing an orbit, the FDF uses this information to generate a
time history of where the satellite was (definitive orbit ) and where it
will be (predicted orbit), and the associated velocity at each time point.
Short term ephemeris is produced for the next week; long ephemeris is
produced for the next month.
- Ephemerides are then transformed into acquisition data in an Improved
Inter-Range Vector (IIRV) format. IIRVs contain satellite position and
velocity, with a reference epoch time.
- Once an orbit is computed, it is also quality checked against a previously
determined orbit to ensure continuity and accuracy.
- IIRVs (commonly called state vectors) are sent to WSC for both
the TDRSs and their customers. Updates to these vectors are normally
provided several times a day .
- WSC uses IIRVs to track the TDR spacecraft and for TDRS antenna pointing
angles necessary to acquire and track the customer spacecraft.
- Differences between the predicted coordinates and the actual coordinates
measured during the support are returned to the FDF as UTDF tracking
messages to update the tracking data base. New updated IIRVs can then be
produced and the cycle begins again.
The TDRSS tracking data format, a subset of the NASA Universal Tracking Data
Format (UTDF), consists of 75 bytes of contiguous information comprising one
sample of data. Tracking data messages (TDMs) consist of one or more standard
NASA/TDRSS 4800 bit data blocks with each block containing from 1 to 7 tracking
samples. The number of samples is a function of simultaneous TDRSS service
support.
TDRSS tracking support can be accessed through any of three types of forward and
return link TDRSS services (MA, SSA, KSA), depending on tracking
requirements. The type of tracking services available depends on the Data Group
and Mode used for support.
Although the minimum requirement for TDRSS tracking support is a single
return link (for one way Doppler support), typical scenarios for TDRSS tracking
support include an active forward and return link to the customer's flight
platform using either the MA, SSA, or KSA services.
Types of TDRSS Nominal tracking support include:
Various sampling rates of Range and Doppler data can be provided for
real-time delivery to the GSFC FDF (e.g., 1/sec., 1/5 sec.)
Customer Requirements for Nominal Tracking Support
- Two Way Ranging For nominal tracking services, the two-way ranging can
only be done when the customer service is coherent, at least one of the
return data channels is PN spread, and the return link PN code is
synchronized with the PN code of the TDRSS forward link received by the
customer S/C.
- Two-way Doppler The two way Doppler (Range Rate) measurement requires a
return link carrier that is coherent with the forward link carrier.
"Coherent" means the return link is coherently related in
frequency (as a function of the customer S/C transponder) to the TDRSS
forward link received by the customer S/C.
- One-way Doppler The one way Doppler measurement only requires an active
return link carrier.
In addition to these nominal services, S-band customers can receive simultaneous
cross-support tracking services which provide two-way Range and Doppler
measurements to customers using either MA or SSA on the forward link and to the
opposite type of S-band service (MA or SSA) on the return link (e.g., the MA on
the forward link crossed with SSA on the return link).
TDRSS tracking support, along with orbit determination provided by the FDF, is
capable of providing 50-100 meter accuracy (week to week) with TDRSS supporting
customer S/C signal Doppler frequencies up to + or - 230 kHz and Doppler rates
up to 1.5 kHz/sec.
Monitoring and correction of S/C attitude (altering of Roll, Pitch, and Yaw
orientation) is the primary responsibility of the customer, with FDF assisting.
Parameters that describe attitude orientation are downlinked within
housekeeping telemetry to customer POCCs which can strip out this data, reformat
it and send it to the FDF. The FDF can provide customers with both real-time and
near-real-time attitude control information based on mission requirements, and
provide this information in the form of commands to the POCC for making attitude
adjustments.
The TDRSs themselves are tracked by the DSMC scheduling tracking services to
ground-based transponders known as the Bilateration Ranging Transponder System (BRTS).
Each TDRS is scheduled twice every four hours to track the BRTS transponders.
Since the BRTS locations are precisely known, the FDF can accurately compute the
TDRS locations. TDRS locations are ,in turn, provided to the customer for their
tracking of the TDRSs.
GSFC has also developed a navigation tool called the TDRSS On-board Navigation
System (TONS) which allows basic tracking measurement data to be computed at the
customer flight platform, instead of on the ground at FDF. TONS produces both
raw radiometric data and orbit determination data on-board through the
combination of a second generation TDRS transponder, and external ultra stable
oscillator (USO) a Doppler extraction card, and on-board navigation and signal
processing software. TONS provides tracking measurement and orbit determination
with little additional cost, weight, and volume impact on the customer's flight
platform.
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