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888-501-2100 • 410-956-8805
Website: www.ATIcourses.com • Email: ATI@ATIcourses.com
http://www.ATIcourses.com/schedule.htm
http://www.aticourses.com/ground_station_design.htm
ATI Course Schedule:
ATI's Ground System Design & Operation:
Professional Development Short Course On:
Ground System Design & Operation
Instructor:
Steve Gemeny
All rights reserved by Steven E. Gemeny 2003, 2004
This material is protected by U.S. copyright laws. Copyright 2009, 2004 Steven E. Gemeny
www.ATIcourses.com
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increases effectiveness and productivity. Learn from the proven best.
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Ground System Design and Operations
Preface
In preparing this presentation I have discovered that it is more
difficult to select meaningful highlights than it is to simply
teach the course. I have attempted to distill over 350 slides
into a cohesive overview of this course.
The challenge has been to provide a smattering of slides that
capture the breadth of the course material without being either
overwhelming in quantity or underwhelming in quality.
Hopefully I have been successful in capturing the essence of
the class.
Ground System Design and Operations
Introduction
In discussing “Spacecraft Ground Systems” a frequent issue
results from the different meaning associated with the term
depending on ones vantage point. In this class I strive to provide
a uniform level of understanding that encompasses the entire
spacecraft ground system, beginning with the reception of radio
signals by the antenna and continuing right through to the display
of telemetry. In this way the student gains a through
understanding of how compromises made in one area affect other
areas of the Ground System. The result is a better understanding
of overall system capabilities and the ability to better optimize
performance.
Ground System Design and Operations
Course Overview
1. The Link Budget: Basic communications principles and
theory; losses, propagation, and system performance
2. Ground Station Architecture and System Design: Ground
station topology, system elements and technology
3. Ground Station Elements: Major subsystems, including their
roles, parameters, limitations, and tradeoffs
4. Figure of Merit (G/T): The key parameter used to
characterize ground station performance, bringing all ground
station elements together as a system
5. Modulation Basics: Signal sets, analog and digital modulation
schemes, and performance parameters
Ground System Design and Operations
Course Overview (Continued)
6. Ranging and Tracking: an introduction to the concepts of
orbital elements sets and a discussion of the acquisition of the
data needed for orbit determination and propagation
7. Ground Station Networks and Standards: Existing and
planned ground station networks and standards including
applicability, advantages, and disadvantages of each
8. CCSDS: A primer on the CCSDS Recommendations for
telecommand and telemetry formats for space missions
including an overview of CFDP
9. Beyond the Ground Station: An overview of ground system
design beyond the boundary of the physical layer
Ground System Design and Operations
Course Overview (Continued)
10. Ground Station Operations: An overview of day-to-day
operations in a typical ground station including general
management, daily planning, pass execution, data processing
and analysis, and maintenance
11. Trends in Ground Station Design: The positive impact of
the “Faster, Better Cheaper” approach on Ground Station
design and operation, including the value added by emergent
COTS hardware and software systems, new trends in
autonomy, and “lights out” operations
Ground System Design and Operations
Link Budget
• A link budget is developed using the generalized Link
Equation and the selected or anticipated link parameters
• This link budget is used to predict either the anticipated link
performance at a specified margin or the anticipated margin at
a specified performance level (e.g., bit rate)
• Link budgets are generally shown as columnar sums which
lend themselves to computer spreadsheets
• A sample Link Budget is shown on the following page; this
Link Budget spreadsheet is available upon request
Ground System Design and Operations
Sample Link Budget Spreadsheet
Transmitter Output Power (W) 5.00
Transmitter Output Power (dBW) 6.99
Feed Losses (dB) -1.50
Transmit Antenna Gain (dB) 1.00
EIRP (dBW) 6.49
Signal Frequency (GHz) 2.25
Path Length (km) 2400.00
Path Loss (dB) -167.09
Absorption Losses (dB) -1.50
Polarization Loss (dB) -0.25
Pointing Loss (dB) -1.00
Recieved Power (dBW) -163.35
Recieve System G/T (dB/K) 23.00
Boltzmann's Constant (dBW/Hz-K) -228.60
Received C/No (dB/Hz) 88.25
Channel Bandwidth (MHz) 50.00
Channel Bandwidth (dB-Hz) 76.99
Received C/N (dB) 11.26
Bit Rate (Mbps) 25.00
Bit Rate (dB-Hz) 73.98
Recieved Eb/No (dB) 14.27
Required Eb/No (dB) 10.50
Link Margin (dB) 3.77
• This sample spreadsheet was developed
using Microsoft Excel
• Parameters shown in shaded boxes are
entered by the user; those in the white
boxes are calculated by Excel
• This spreadsheet gives performance in a
variety of parameters including C/N,
C/No, and Eb/No, each of which is
applicable to a different type of link;
these will be covered in detail
Ground System Design and Operations
Ground Station Block Diagram
Diplexer DownconverterLNA Demodulator
UpconverterHPA Modulator
Downlink
Data
Uplink
Data
Antenna
Control Signal Strength
Ref
OscFeed
System
Antenna
System
Pedestal
System
Tuning
Synthesizer
Control System
Ground System Design and Operations
G/T Model
• To understand G/T, it is useful to have a system model where
each contribution to G/T can be mapped out and intuitively
understood, as shown in the figure below:
Diplexer etc...
Reference Point
D/C
Tsky
Tatmosphere
Tinterference
Tcoax
Gcoax
Tcoax
Gcoax
Tdiplexer
Gdiplexer
THPA
TLNA
GLNA Gdownconverter
Tdownconverter
Gantenna
Tantenna
Ground System Design and Operations
Noise due to Subsequent Gain Stages
• Since the noise contribution of all gain stages must be
reflected back to the reference point, the noise contribution of
each stage must be divided by the gain of earlier stages to
represent an equivalent noise source at the reference
• For three gain stages following the LNA of G1, T1, G2, T2, G3,
and T3, the equivalent total noise temperature is:
Tequivalent = TLNA +
T1
GLNA
+
T2
GLNAG1
+
T3
GLNA G1G2
GLNA
TLNA
Reference
Point
G1
T1
G2
T2
G3
T3
Ground System Design and Operations
A Sample Spreadsheet Calculation
Gain (dB) Temp (K) Temp (dBK) Loss (dB) Tref (dBK) Gref (dB) Tref (K)
Antenna 23.50 90.00 19.54 -1.45 18.09 23.50 64.45
Coaxial Cable -0.50 31.54 14.99 -0.95 14.04 -0.50 25.34
Diplexer -0.85 51.55 17.12 -0.10 17.02 -0.85 50.38
HPA Leakage 72.46 18.60 -0.10 18.50 70.81
Coaxial Cable -0.10 6.60 8.20 0.00 8.20 -0.10 6.60
Reference Point
LNA 30.00 62.69 17.97 0.00 17.97 62.69
Downconverter 30.00 2610.00 34.17 -30.00 4.17 2.61
LNA Noise Figure (dB) 0.85 G (dB) T (K)
Downconverter Noise Figure (dB) 10.00 Totals: 22.05 282.89
HPA In-band Noise (dBW/Hz) -90.00
HPA Temperature (dBK) 138.60
Diplexer Isolation, TX-RX (dB) -120.00
HPA Leakage (dBK) 18.60
HPA Leakage (K) 72.46 G (dB) 22.05
T (dBK) 24.52
Ambient Temperature (K) 290.00
Boltzmann's Constant (dBW/Hz-K) -228.60 G/T (dB/K) -2.47
Reference G/T model depicted on page 4-5
Ground System Design and Operations
Ground Station Components
This section will proceed through a typical Ground Station
subsystem by subsystem, as outlined previously in Section 2,
breaking each subsystem into components and describing each of
those parts in a much greater level of detail
Ground System Design and Operations
Antenna Systems
• The antenna system is synonymous with the Ground Station in
the eyes of most neophytes; who can think of a ground station
without picturing a large antenna, generally a parabolic
reflector or “antenna dish”?
• Accordingly, this first section will be devoted to antenna
systems and antenna designs and characteristics
• Before beginning any detailed discussion of antenna
subsystems, it is important to define some key parameters
Ground System Design and Operations
Antenna Temperature
• An antenna exhibits a certain antenna temperature (TA); this is
the temperature of a blackbody which would produce an
equivalent noise power as the antenna
• TA is a function of antenna pattern, the surrounding
environment, and the direction of antenna pointing; for a
highly directional antenna pointed at “cold” space, the noise
power coupling into the back lobe of the antenna from the
“hot” earth has little effect on the overall low TA
• TA is an important factor in overall ground station G/T
TA = G(θ,φ)T(θ,φ)dθdφ∫∫
Ground System Design and Operations
Dish Gain Derivation
G = Ae
4π
λ2 G = ηA
4π
λ2 G = ηπr2 4π
λ2⇒ ⇒
G = ηπ
D
2
⎛
⎝
⎜
⎞
⎠
⎟
2
4π
λ2 G = η
4D2
π2
4λ2
⇒ ⇒
G = η
Dπ
λ
⎛
⎝
⎜
⎞
⎠
⎟
2
G = η
D2
π2
λ2
⇒ ⇒
Ground System Design and Operations
Antenna Pointing and Tracking
Systems
• A large or high gain antenna must be carefully pointed to
receive energy from a desired spacecraft; this can be compared
to observing a target through a soda straw or high-
magnification telescope. If the target is not in the field of
view, the signal will not be received.
• The purpose of the antenna pointing and tracking system is to
acquire the satellite, or get it into the field of view of the
antenna, and track the satellite, i.e., keep the spacecraft in the
field of view or main beam of the antenna so that data can be
transmitted and received both ways
Ground System Design and Operations
Antenna Pointing and Tracking
Systems
• There are three common methods for pointing and tracking an
antenna system for a ground station:
– Open Loop
– Step Track
– Monopulse
• Each of these pointing and tracking systems will be described
in greater detail in the charts which follow; while these
systems are not all-encompassing, they account for most
commercially developed and built ground stations
Ground System Design and Operations
Low Noise Amplifiers
• In the next section, we will discuss the calculation of the
ground station Figure of Merit, or G/T, which is a key
parameter in establishing a ground station’s performance
• In G/T, it will become clear that the noise performance of the
first active gain stage in the ground station is absolutely
critical in establishing the system’s performance level
• This first gain stage is called the Low-Noise Amplifier, or
LNA; improvements in LNA performance have driven
improvements in ground station performance and utility more
than any other single area of technology development
Ground System Design and Operations
High Power Amplifiers
• The last active device in the transmit chain before the antenna
feed assembly is the Power Amplifier (PA), also frequently
referred to as the High Power Amplifier (HPA)
• There are three major types of HPA commonly in use in
Ground Station transmission systems today:
– Traveling Wave Tube Amplifiers (TWTAs)
– Klystrons
– Solid State Power Amplifiers (SSPAs)
• Each will be briefly described in the charts that follow
Ground System Design and Operations
Frequency Conversion
• The modulation and demodulation of data carrying signals
tends to be performed at relatively low frequencies in the 10-
400 MHz range for reasons of convenience; design topologies
and components that operate properly in this frequency band
are well understood and easily fabricated
• Transmission of carriers tends to be in the 1-40 GHz range for
space communications due to the availability of bandwidth and
the physics of atmospheric propagation
• As long as this continues to be the common practice,
frequency conversion systems will continue to be needed
Ground System Design and Operations
Understanding Modulation Basics
• An unmodulated signal, or carrier conveys no information
• To be useful, it is necessary to modulate the carrier, i.e., to
vary some element of the carrier in a way that information is
conveyed and can be recovered by the demodulator
• An RF signal, or carrier, has several characteristics that can be
modulated in a manner that can be detected so the original
modulating signal can be reproduced, including:
– Amplitude
– Frequency
– Phase
Ground System Design and Operations
Phase Modulation
• In Phase Modulation, or
PM, the phase of the carrier
is modulated as a function
of the input signal
• The PM signal can be
described mathematically:
where φ(t) is the
modulating signal
F(t ) = Asin(ωt + φ(t))
Ground System Design and Operations
Digital Communications Overview
Original
Signal
Sampling Quantizing Encoding Transmission
Reproduced
Signal
Filtering
Digital-to-
Analog
Conversion
Decoding Reception
Bandlimiting
8, 34, 51,
50, 36, 11,
-41, -50,
-48, -38, ...
001101101
100010101
001100010
10100010...
8, 34, 51,
50, 36, 11,
-41, -50,
-48, -38, ...
001101101
100010101
001100010
10100010...
Ground System Design and Operations
Signal Constellation Examples
• It is useful at this time to represent signal constellations in
phase and amplitude space; each symbol, which has its own
phase and amplitude, corresponds to a number of bits
• Errors are generated when the vector addition of noise causes
the resultant signal to cross a decision boundary into the signal
space of another symbol, resulting in errors
0°
90°
180°
-90°BPSK
0°
90°
180°
-90°QPSK
0°
90°
180°
-90°QAM
0°
90°
180°
-90°8-ary PSK
01 0011
01
10
Decision
Boundary
000
001011
010
100
101111
110
Decision
Boundary
Decision
Boundary
Ground System Design and Operations
CCSDS Telecommand System
Layers
Ground System Design and Operations
Telecommand Data Structures
Ground System Design and Operations
Telemetry Transfer Frame Format
Ground System Design and Operations
CFDP At A Glance
Ground System Design and Operations
Convolutional Encoder
• The Encoder pictured below with constraint length N = 3 and
ν = 2 modulo 2 adders will produce the output code sequence
shown in response to the input sequence below
d1 d2 d3
+
+
s1 = d1 ⊕ d2 ⊕ d3
d1 d2 d3 s1 s2
0 0 0 0 0
1 0 0 1 1
1 1 0 0 1
0 1 1 0 1
1 0 1 0 0
0 1 0 1 0
0 0 1 1 1
0 0 0 0 0
s2 = d1 ⊕ d3
Input
Sequence
11010
Ouput
Sequence
0011010100101100
Data In Data Out
= Modulo 2 addition = XOR+
Ground System Design and Operations
Ground System Block Diagram
USER
Command
Generator
Telemetry
Interpreter
Command
Dictionary
Telemetry
Dictionary
Command
Packetizer
Command
Framer
Command
Encoder
Command
Exciter
Diplexer
Receiver
Bit
Sync
Telemetry
Decoder
Channel
Separator
Telemetry
Deframer
Ground
Station
Front
End
MOC
HW/SW
TLM
VCs
TLM
Frames
TLM
Clk & Data
CLTUs
TC
Frames
TC
Packets
TLM
Packets
CMD
Language
LNA
HPA
Ground System Design and Operations
TIMED End to End Data System*
Symbol Key
Op
Operator I/F
Hardware or
Hdw/Software
Software
Receiver
Transmitter
RF
RF
Bit-Serial
CCSDS
Frames
Ground Station (pre-launch & on-orbit)
S/C Command &Data Handling (C&DH) Subsystem PCI Spacecraft Subsys
Execute
Tlm (Transfer Frames)
Bus
Transport
Control
Cmd Pkt
Tlm PktControl
Subsystem
of the C&DH
POC (1 of 4)
Mission Data Center
Ingest
Tlm
RF GSERF
Ground Support Equipment (pre-launch)
Operate
S/C Bus
&
Ground
Sys
Instrument Cmd Msg
Instrument Cmd Packet
Bit-Serial CCSDS Frames
Umbilical
Adapter
Retrieve
Tlm
Normal Cmds (CLTU)
‘Hard-wired’
Critical Cmds
(VC 0,1)
Co-Investigators
Public
Bus
Cmd Packet
Dump
Packet
Instrmt, Subsys R-T Tlm Pkt
R-T Packet Stream
Selected Tlm Product
CCSDS
TC
Frames
PCI Bus
Transport
Control
Collect
R-T
Tlm
CCSDS
Packet
Transport
Service
Bus
Housekeeping Pkt
Ground Equipment Control
Normal
Cmd
Frames
(VC 2,3)
Instrumt. Cmd Pkts
R-T Tlm
Pkt Stream
Serve
Products
Internet (or Equiv)
Op
Bus Command
Packets
R-T
Frames
Other Bus
Op
Front
End
(ftp/http)
Terminal
Ingest
Products
Data
Storage
Data
Analysis
Stimulus
GSE
RF Sys.
with
Uplink I/F
CCSDS
Packet
Transport
Service
(ftp/http)
Terminal
Front
End
Science
Products
Archive
Telemetry
Archive
PJG, rev e, 2-7-97
Internet
Protocol
(TCP/IP)
CLTU
Bit-Serial
CCSDS
Frames
CLTU
CCSDS
Frame
Handling
Dump
Frames
(VC 6)
R-T
Frames
(VC 7)
1553 Spacecraft Subsys
Execute
Bus
Transport
Control
Cmd Pkt
Tlm Pkt
Instrument (1 of 4)
Execute
Bus
Transport
Control
Cmd Pkt
Tlm Pkt
Mission Operations Center
Dump
Frames
Command ReceiptHskp. R-T Packets
Authenticate,
Log, and
Forward
Serve Tlm
Telemetry
Storage
CCSDS
Packet
Transport
Service
Operate
Instrument
& GSE
1553
Bus
Transport
Control
* End to End Data System Figure courtesy of P. J. Grunberger, The Johns Hopkins University Applied Physics Laboratory
Register online at www.aticourses.com or call ATI at 888.501.2100 or 410.531.6034
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with On-Site Courses
Tailored toYour Needs
The Applied Technology Institute specializes in training programs for technical
professionals. Our courses keep you current in the state-of-the-art technology that is
essential to keep your company on the cutting edge in today’s highly competitive
marketplace. For 20 years, we have earned the trust of training departments nationwide,
and have presented on-site training at the major Navy, Air Force and NASA centers, and for a
large number of contractors. Our training increases effectiveness and productivity. Learn
from the proven best.
ATI’s on-site courses offer these cost-effective advantages:
• You design, control, and schedule the course.
• Since the program involves only your personnel, confidentiality is maintained. You can
freely discuss company issues and programs. Classified programs can also be arranged.
• Your employees may attend all or only the most relevant part of the course.
• Our instructors are the best in the business, averaging 25 to 35 years of practical, real-
world experience. Carefully selected for both technical expertise and teaching ability, they
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We suggest you look at ATI course descriptions in this catalog and on the ATI website.
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of our courses in these areas:
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I suggest that you read through these course descriptions and then call me personally, Jim
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Ground_System_Design_&_Operation

  • 1. 349 Berkshire Drive • Riva, Maryland 21140 888-501-2100 • 410-956-8805 Website: www.ATIcourses.com • Email: ATI@ATIcourses.com http://www.ATIcourses.com/schedule.htm http://www.aticourses.com/ground_station_design.htm ATI Course Schedule: ATI's Ground System Design & Operation: Professional Development Short Course On: Ground System Design & Operation Instructor: Steve Gemeny All rights reserved by Steven E. Gemeny 2003, 2004 This material is protected by U.S. copyright laws. Copyright 2009, 2004 Steven E. Gemeny
  • 2. www.ATIcourses.com Boost Your Skills with On-Site Courses Tailored to Your Needs The Applied Technology Institute specializes in training programs for technical professionals. Our courses keep you current in the state-of-the-art technology that is essential to keep your company on the cutting edge in today’s highly competitive marketplace. Since 1984, ATI has earned the trust of training departments nationwide, and has presented on-site training at the major Navy, Air Force and NASA centers, and for a large number of contractors. Our training increases effectiveness and productivity. Learn from the proven best. For a Free On-Site Quote Visit Us At: http://www.ATIcourses.com/free_onsite_quote.asp For Our Current Public Course Schedule Go To: http://www.ATIcourses.com/schedule.htm 349 Berkshire Drive Riva, Maryland 21140 Telephone 1-888-501-2100 / (410) 965-8805 Fax (410) 956-5785 Email: ATI@ATIcourses.com
  • 3. Ground System Design and Operations Preface In preparing this presentation I have discovered that it is more difficult to select meaningful highlights than it is to simply teach the course. I have attempted to distill over 350 slides into a cohesive overview of this course. The challenge has been to provide a smattering of slides that capture the breadth of the course material without being either overwhelming in quantity or underwhelming in quality. Hopefully I have been successful in capturing the essence of the class.
  • 4. Ground System Design and Operations Introduction In discussing “Spacecraft Ground Systems” a frequent issue results from the different meaning associated with the term depending on ones vantage point. In this class I strive to provide a uniform level of understanding that encompasses the entire spacecraft ground system, beginning with the reception of radio signals by the antenna and continuing right through to the display of telemetry. In this way the student gains a through understanding of how compromises made in one area affect other areas of the Ground System. The result is a better understanding of overall system capabilities and the ability to better optimize performance.
  • 5. Ground System Design and Operations Course Overview 1. The Link Budget: Basic communications principles and theory; losses, propagation, and system performance 2. Ground Station Architecture and System Design: Ground station topology, system elements and technology 3. Ground Station Elements: Major subsystems, including their roles, parameters, limitations, and tradeoffs 4. Figure of Merit (G/T): The key parameter used to characterize ground station performance, bringing all ground station elements together as a system 5. Modulation Basics: Signal sets, analog and digital modulation schemes, and performance parameters
  • 6. Ground System Design and Operations Course Overview (Continued) 6. Ranging and Tracking: an introduction to the concepts of orbital elements sets and a discussion of the acquisition of the data needed for orbit determination and propagation 7. Ground Station Networks and Standards: Existing and planned ground station networks and standards including applicability, advantages, and disadvantages of each 8. CCSDS: A primer on the CCSDS Recommendations for telecommand and telemetry formats for space missions including an overview of CFDP 9. Beyond the Ground Station: An overview of ground system design beyond the boundary of the physical layer
  • 7. Ground System Design and Operations Course Overview (Continued) 10. Ground Station Operations: An overview of day-to-day operations in a typical ground station including general management, daily planning, pass execution, data processing and analysis, and maintenance 11. Trends in Ground Station Design: The positive impact of the “Faster, Better Cheaper” approach on Ground Station design and operation, including the value added by emergent COTS hardware and software systems, new trends in autonomy, and “lights out” operations
  • 8. Ground System Design and Operations Link Budget • A link budget is developed using the generalized Link Equation and the selected or anticipated link parameters • This link budget is used to predict either the anticipated link performance at a specified margin or the anticipated margin at a specified performance level (e.g., bit rate) • Link budgets are generally shown as columnar sums which lend themselves to computer spreadsheets • A sample Link Budget is shown on the following page; this Link Budget spreadsheet is available upon request
  • 9. Ground System Design and Operations Sample Link Budget Spreadsheet Transmitter Output Power (W) 5.00 Transmitter Output Power (dBW) 6.99 Feed Losses (dB) -1.50 Transmit Antenna Gain (dB) 1.00 EIRP (dBW) 6.49 Signal Frequency (GHz) 2.25 Path Length (km) 2400.00 Path Loss (dB) -167.09 Absorption Losses (dB) -1.50 Polarization Loss (dB) -0.25 Pointing Loss (dB) -1.00 Recieved Power (dBW) -163.35 Recieve System G/T (dB/K) 23.00 Boltzmann's Constant (dBW/Hz-K) -228.60 Received C/No (dB/Hz) 88.25 Channel Bandwidth (MHz) 50.00 Channel Bandwidth (dB-Hz) 76.99 Received C/N (dB) 11.26 Bit Rate (Mbps) 25.00 Bit Rate (dB-Hz) 73.98 Recieved Eb/No (dB) 14.27 Required Eb/No (dB) 10.50 Link Margin (dB) 3.77 • This sample spreadsheet was developed using Microsoft Excel • Parameters shown in shaded boxes are entered by the user; those in the white boxes are calculated by Excel • This spreadsheet gives performance in a variety of parameters including C/N, C/No, and Eb/No, each of which is applicable to a different type of link; these will be covered in detail
  • 10. Ground System Design and Operations Ground Station Block Diagram Diplexer DownconverterLNA Demodulator UpconverterHPA Modulator Downlink Data Uplink Data Antenna Control Signal Strength Ref OscFeed System Antenna System Pedestal System Tuning Synthesizer Control System
  • 11. Ground System Design and Operations G/T Model • To understand G/T, it is useful to have a system model where each contribution to G/T can be mapped out and intuitively understood, as shown in the figure below: Diplexer etc... Reference Point D/C Tsky Tatmosphere Tinterference Tcoax Gcoax Tcoax Gcoax Tdiplexer Gdiplexer THPA TLNA GLNA Gdownconverter Tdownconverter Gantenna Tantenna
  • 12. Ground System Design and Operations Noise due to Subsequent Gain Stages • Since the noise contribution of all gain stages must be reflected back to the reference point, the noise contribution of each stage must be divided by the gain of earlier stages to represent an equivalent noise source at the reference • For three gain stages following the LNA of G1, T1, G2, T2, G3, and T3, the equivalent total noise temperature is: Tequivalent = TLNA + T1 GLNA + T2 GLNAG1 + T3 GLNA G1G2 GLNA TLNA Reference Point G1 T1 G2 T2 G3 T3
  • 13. Ground System Design and Operations A Sample Spreadsheet Calculation Gain (dB) Temp (K) Temp (dBK) Loss (dB) Tref (dBK) Gref (dB) Tref (K) Antenna 23.50 90.00 19.54 -1.45 18.09 23.50 64.45 Coaxial Cable -0.50 31.54 14.99 -0.95 14.04 -0.50 25.34 Diplexer -0.85 51.55 17.12 -0.10 17.02 -0.85 50.38 HPA Leakage 72.46 18.60 -0.10 18.50 70.81 Coaxial Cable -0.10 6.60 8.20 0.00 8.20 -0.10 6.60 Reference Point LNA 30.00 62.69 17.97 0.00 17.97 62.69 Downconverter 30.00 2610.00 34.17 -30.00 4.17 2.61 LNA Noise Figure (dB) 0.85 G (dB) T (K) Downconverter Noise Figure (dB) 10.00 Totals: 22.05 282.89 HPA In-band Noise (dBW/Hz) -90.00 HPA Temperature (dBK) 138.60 Diplexer Isolation, TX-RX (dB) -120.00 HPA Leakage (dBK) 18.60 HPA Leakage (K) 72.46 G (dB) 22.05 T (dBK) 24.52 Ambient Temperature (K) 290.00 Boltzmann's Constant (dBW/Hz-K) -228.60 G/T (dB/K) -2.47 Reference G/T model depicted on page 4-5
  • 14. Ground System Design and Operations Ground Station Components This section will proceed through a typical Ground Station subsystem by subsystem, as outlined previously in Section 2, breaking each subsystem into components and describing each of those parts in a much greater level of detail
  • 15. Ground System Design and Operations Antenna Systems • The antenna system is synonymous with the Ground Station in the eyes of most neophytes; who can think of a ground station without picturing a large antenna, generally a parabolic reflector or “antenna dish”? • Accordingly, this first section will be devoted to antenna systems and antenna designs and characteristics • Before beginning any detailed discussion of antenna subsystems, it is important to define some key parameters
  • 16. Ground System Design and Operations Antenna Temperature • An antenna exhibits a certain antenna temperature (TA); this is the temperature of a blackbody which would produce an equivalent noise power as the antenna • TA is a function of antenna pattern, the surrounding environment, and the direction of antenna pointing; for a highly directional antenna pointed at “cold” space, the noise power coupling into the back lobe of the antenna from the “hot” earth has little effect on the overall low TA • TA is an important factor in overall ground station G/T TA = G(θ,φ)T(θ,φ)dθdφ∫∫
  • 17. Ground System Design and Operations Dish Gain Derivation G = Ae 4π λ2 G = ηA 4π λ2 G = ηπr2 4π λ2⇒ ⇒ G = ηπ D 2 ⎛ ⎝ ⎜ ⎞ ⎠ ⎟ 2 4π λ2 G = η 4D2 π2 4λ2 ⇒ ⇒ G = η Dπ λ ⎛ ⎝ ⎜ ⎞ ⎠ ⎟ 2 G = η D2 π2 λ2 ⇒ ⇒
  • 18. Ground System Design and Operations Antenna Pointing and Tracking Systems • A large or high gain antenna must be carefully pointed to receive energy from a desired spacecraft; this can be compared to observing a target through a soda straw or high- magnification telescope. If the target is not in the field of view, the signal will not be received. • The purpose of the antenna pointing and tracking system is to acquire the satellite, or get it into the field of view of the antenna, and track the satellite, i.e., keep the spacecraft in the field of view or main beam of the antenna so that data can be transmitted and received both ways
  • 19. Ground System Design and Operations Antenna Pointing and Tracking Systems • There are three common methods for pointing and tracking an antenna system for a ground station: – Open Loop – Step Track – Monopulse • Each of these pointing and tracking systems will be described in greater detail in the charts which follow; while these systems are not all-encompassing, they account for most commercially developed and built ground stations
  • 20. Ground System Design and Operations Low Noise Amplifiers • In the next section, we will discuss the calculation of the ground station Figure of Merit, or G/T, which is a key parameter in establishing a ground station’s performance • In G/T, it will become clear that the noise performance of the first active gain stage in the ground station is absolutely critical in establishing the system’s performance level • This first gain stage is called the Low-Noise Amplifier, or LNA; improvements in LNA performance have driven improvements in ground station performance and utility more than any other single area of technology development
  • 21. Ground System Design and Operations High Power Amplifiers • The last active device in the transmit chain before the antenna feed assembly is the Power Amplifier (PA), also frequently referred to as the High Power Amplifier (HPA) • There are three major types of HPA commonly in use in Ground Station transmission systems today: – Traveling Wave Tube Amplifiers (TWTAs) – Klystrons – Solid State Power Amplifiers (SSPAs) • Each will be briefly described in the charts that follow
  • 22. Ground System Design and Operations Frequency Conversion • The modulation and demodulation of data carrying signals tends to be performed at relatively low frequencies in the 10- 400 MHz range for reasons of convenience; design topologies and components that operate properly in this frequency band are well understood and easily fabricated • Transmission of carriers tends to be in the 1-40 GHz range for space communications due to the availability of bandwidth and the physics of atmospheric propagation • As long as this continues to be the common practice, frequency conversion systems will continue to be needed
  • 23. Ground System Design and Operations Understanding Modulation Basics • An unmodulated signal, or carrier conveys no information • To be useful, it is necessary to modulate the carrier, i.e., to vary some element of the carrier in a way that information is conveyed and can be recovered by the demodulator • An RF signal, or carrier, has several characteristics that can be modulated in a manner that can be detected so the original modulating signal can be reproduced, including: – Amplitude – Frequency – Phase
  • 24. Ground System Design and Operations Phase Modulation • In Phase Modulation, or PM, the phase of the carrier is modulated as a function of the input signal • The PM signal can be described mathematically: where φ(t) is the modulating signal F(t ) = Asin(ωt + φ(t))
  • 25. Ground System Design and Operations Digital Communications Overview Original Signal Sampling Quantizing Encoding Transmission Reproduced Signal Filtering Digital-to- Analog Conversion Decoding Reception Bandlimiting 8, 34, 51, 50, 36, 11, -41, -50, -48, -38, ... 001101101 100010101 001100010 10100010... 8, 34, 51, 50, 36, 11, -41, -50, -48, -38, ... 001101101 100010101 001100010 10100010...
  • 26. Ground System Design and Operations Signal Constellation Examples • It is useful at this time to represent signal constellations in phase and amplitude space; each symbol, which has its own phase and amplitude, corresponds to a number of bits • Errors are generated when the vector addition of noise causes the resultant signal to cross a decision boundary into the signal space of another symbol, resulting in errors 0° 90° 180° -90°BPSK 0° 90° 180° -90°QPSK 0° 90° 180° -90°QAM 0° 90° 180° -90°8-ary PSK 01 0011 01 10 Decision Boundary 000 001011 010 100 101111 110 Decision Boundary Decision Boundary
  • 27. Ground System Design and Operations CCSDS Telecommand System Layers
  • 28. Ground System Design and Operations Telecommand Data Structures
  • 29. Ground System Design and Operations Telemetry Transfer Frame Format
  • 30. Ground System Design and Operations CFDP At A Glance
  • 31. Ground System Design and Operations Convolutional Encoder • The Encoder pictured below with constraint length N = 3 and ν = 2 modulo 2 adders will produce the output code sequence shown in response to the input sequence below d1 d2 d3 + + s1 = d1 ⊕ d2 ⊕ d3 d1 d2 d3 s1 s2 0 0 0 0 0 1 0 0 1 1 1 1 0 0 1 0 1 1 0 1 1 0 1 0 0 0 1 0 1 0 0 0 1 1 1 0 0 0 0 0 s2 = d1 ⊕ d3 Input Sequence 11010 Ouput Sequence 0011010100101100 Data In Data Out = Modulo 2 addition = XOR+
  • 32. Ground System Design and Operations Ground System Block Diagram USER Command Generator Telemetry Interpreter Command Dictionary Telemetry Dictionary Command Packetizer Command Framer Command Encoder Command Exciter Diplexer Receiver Bit Sync Telemetry Decoder Channel Separator Telemetry Deframer Ground Station Front End MOC HW/SW TLM VCs TLM Frames TLM Clk & Data CLTUs TC Frames TC Packets TLM Packets CMD Language LNA HPA
  • 33. Ground System Design and Operations TIMED End to End Data System* Symbol Key Op Operator I/F Hardware or Hdw/Software Software Receiver Transmitter RF RF Bit-Serial CCSDS Frames Ground Station (pre-launch & on-orbit) S/C Command &Data Handling (C&DH) Subsystem PCI Spacecraft Subsys Execute Tlm (Transfer Frames) Bus Transport Control Cmd Pkt Tlm PktControl Subsystem of the C&DH POC (1 of 4) Mission Data Center Ingest Tlm RF GSERF Ground Support Equipment (pre-launch) Operate S/C Bus & Ground Sys Instrument Cmd Msg Instrument Cmd Packet Bit-Serial CCSDS Frames Umbilical Adapter Retrieve Tlm Normal Cmds (CLTU) ‘Hard-wired’ Critical Cmds (VC 0,1) Co-Investigators Public Bus Cmd Packet Dump Packet Instrmt, Subsys R-T Tlm Pkt R-T Packet Stream Selected Tlm Product CCSDS TC Frames PCI Bus Transport Control Collect R-T Tlm CCSDS Packet Transport Service Bus Housekeeping Pkt Ground Equipment Control Normal Cmd Frames (VC 2,3) Instrumt. Cmd Pkts R-T Tlm Pkt Stream Serve Products Internet (or Equiv) Op Bus Command Packets R-T Frames Other Bus Op Front End (ftp/http) Terminal Ingest Products Data Storage Data Analysis Stimulus GSE RF Sys. with Uplink I/F CCSDS Packet Transport Service (ftp/http) Terminal Front End Science Products Archive Telemetry Archive PJG, rev e, 2-7-97 Internet Protocol (TCP/IP) CLTU Bit-Serial CCSDS Frames CLTU CCSDS Frame Handling Dump Frames (VC 6) R-T Frames (VC 7) 1553 Spacecraft Subsys Execute Bus Transport Control Cmd Pkt Tlm Pkt Instrument (1 of 4) Execute Bus Transport Control Cmd Pkt Tlm Pkt Mission Operations Center Dump Frames Command ReceiptHskp. R-T Packets Authenticate, Log, and Forward Serve Tlm Telemetry Storage CCSDS Packet Transport Service Operate Instrument & GSE 1553 Bus Transport Control * End to End Data System Figure courtesy of P. J. Grunberger, The Johns Hopkins University Applied Physics Laboratory
  • 34. Register online at www.aticourses.com or call ATI at 888.501.2100 or 410.531.6034 BoostYour Skills with On-Site Courses Tailored toYour Needs The Applied Technology Institute specializes in training programs for technical professionals. Our courses keep you current in the state-of-the-art technology that is essential to keep your company on the cutting edge in today’s highly competitive marketplace. For 20 years, we have earned the trust of training departments nationwide, and have presented on-site training at the major Navy, Air Force and NASA centers, and for a large number of contractors. Our training increases effectiveness and productivity. Learn from the proven best. ATI’s on-site courses offer these cost-effective advantages: • You design, control, and schedule the course. • Since the program involves only your personnel, confidentiality is maintained. You can freely discuss company issues and programs. Classified programs can also be arranged. • Your employees may attend all or only the most relevant part of the course. • Our instructors are the best in the business, averaging 25 to 35 years of practical, real- world experience. Carefully selected for both technical expertise and teaching ability, they provide information that is practical and ready to use immediately. • Our on-site programs can save your facility 30% to 50%, plus additional savings by eliminating employee travel time and expenses. • The ATI Satisfaction Guarantee: You must be completely satisfied with our program. We suggest you look at ATI course descriptions in this catalog and on the ATI website. Visit and bookmark ATI’s website at http://www.ATIcourses.com for descriptions of all of our courses in these areas: • Communications & Computer Programming • Radar/EW/Combat Systems • Signal Processing & Information Technology • Sonar & Acoustic Engineering • Spacecraft & Satellite Engineering I suggest that you read through these course descriptions and then call me personally, Jim Jenkins, at (410) 531-6034, and I’ll explain what we can do for you, what it will cost, and what you can expect in results and future capabilities. Our training helps you and your organization remain competitive in this changing world.