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Dave Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

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Spacecraft Communication. Dave Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville) Dream Chaser Principle Systems Engineer for Comm & Instrumentation Space Shuttle Program Shuttle Avionics Integration Lab Test Engineer (JSC, Houston) - PowerPoint PPT Presentation
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Dave Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville) Dream Chaser Principle Systems Engineer for Comm & Instrumentatio Space Shuttle Program Shuttle Avionics Integration Lab Test Engineer (JSC, Houston) Flight Design Engineer for Rendezvous/Prox Ops (JSC, Houston) OV 105 Final Assembly Test Engineer (AF Plant 42 Palmdale, Ca) Crew/Flt Controller Training (JSC, Houston) • Comm/Instrumentation • Control/Propulsion Training Lead Simulation Supervisor Spacecraft Communication
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Page 1: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

Dave Pitre

•Sierra Nevada Corporation( Space Exploration Systems, Louisville)• Dream Chaser Principle Systems Engineer for Comm & Instrumentation

•Space Shuttle Program• Shuttle Avionics Integration Lab Test Engineer (JSC, Houston)• Flight Design Engineer for Rendezvous/Prox Ops (JSC, Houston)• OV 105 Final Assembly Test Engineer (AF Plant 42 Palmdale, Ca)• Crew/Flt Controller Training (JSC, Houston)

• Comm/Instrumentation• Control/Propulsion• Training Lead• Simulation Supervisor

Spacecraft Communication

Page 2: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

Spacecraft Communication

Page 3: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

What does a spacecraft communication systems engineer do?

•Analyze Comm System Requirements

•Design Comm System Architecture

•Procure Comm System Hardware/Software

•Test Comm System Hardware/Software

•Integrate Comm System Hardware/Software

•Install/Test Comm System Hardware/Software

•Maintain Comm System Hardware/Software

•Train Comm System Hardware/Software

Page 4: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

Commands

Voice

CommunicationNetworks

Satellite/Ground

MCC

Data/TelemetryRF

Systems

Video

Systems Level Overview

Page 5: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

Challenges Unique to Space Communication

•Distance

• Speed

•Line of sight

•Ground Track

•Earth surface radiation limit

•Limited number of users

Page 6: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

USA004460Basic

Ground Station Line of Sight

AOS Acquisition of Signal

LOS Loss of Signal

UPLINK

DOWNLINK

Horizo

n line

126

Page 7: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

57

Page 8: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

DFR

DGS

VTS

TCS

WLPMILA and

PDL

CTSNHS

HTS

GTS

Orbit Ground Precession

Page 9: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

TDRS EAST and WEST COVERAGE

TDRSEASTTDRS

WEST

TDRS Z

AtlanticPacific

Indian Ocean

ZOE:

ZONE OF EXCLUSION

(LASTS 5-15 MINUTES)

USA004460Rev A

Page 10: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

Practical Examples

TrackingDataRelaySatellite

MCC

Telemetry

Commands

GSTDN

GSFC

AFSCNARTS

WSC

Telemetry

Commands

Page 11: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

Practical Examples

Payload

MCC

Downlink

Uplink

CommandsTelemetry

GSTDN

EVA

GSFC

AFSCNARTS

Voice

Data

Page 12: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

Practical Examples

Payload

TrackingDataRelaySatellite

MCC

DownlinkDownlinkUplink

Uplink

Commands

Commands/Data/VoiceTelemetry

Telemetry/Data/Voice

GSTDN

EVA

GSFC

AFSCNARTS

WSC

Voice

Data

Page 13: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

Practical Examples

Payload

TrackingDataRelaySatellite

MCC

DownlinkDownlinkUplink

Uplink

Commands

Commands/Data/VoiceTelemetry

Telemetry/Data/Voice

GSTDN

Space Station

EVA

GSFC

AFSCNARTS

WSC

Commands/Data/VoiceTelemetry/Data/Voice

Voice

Data

Page 14: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

RF Overview Electromagnetic Waves

• Light, electromagnetic waves, radiation = electromagnetic energy.

• This energy can be described by frequency, wavelength, or energy.

• Radio usually described in terms of frequency (Hertz).

Page 15: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

RF Overview Modulation and Waveforms

Modulation Data

Amplitude Modulation

Freq Modulation

Page 16: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

RF Overview Time, Frequency, Phase Domain

Page 17: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

Power is used to quantify a signal, instead of amplitude, and is expressed in Watts.

For low-frequency signals, the power is given by P = IE

RF Overview Signal Power

Page 18: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

RF Overview Signal Power

Transmitter Power Output In radio transmission, transmitter power output (TPO) is the actual amount of power (in watts) of radio frequency (RF) energy that a transmitter produces at its output.

Effective Isotropic Radiated Power Power that comes off an antenna is measured as effective isotropic radiated power (EIRP). EIRP is the value that regulatory agencies, such as the FCC, use to determine and measure power limits in applications.

TransmitterTPO EIRP

cable

Page 19: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

RF Overview Decibels

• The decibel is a unitless method of expressing the ratio of two quantities.

• The expression is in terms of the logarithm to base 10 of the ratio instead of

the raw ratio.

• This is done for convenience in expressing the ratio of numbers many

magnitudes apart with decibel numbers that are not as large.

PdBm=10log10(Pwatts/1mW)

Page 20: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

RF Overview Decibels

The advantage of using decibels instead of Watts to express the power of a signal along an RF is that instead of dividing or multiplying powers to take care of amplifications and attenuations, we just add or subtract the gains and the losses expressed in decibels

TransmitterTPO EIRP

cable

Page 21: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

RF Overview Analog v. Digital

Page 22: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

RF Overview Analog v. Digital

Page 23: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

RF Overview Analog v. Digital

Analog to Digital Conversion (A/D)

Page 24: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

RF Overview Signal to Noise Ratio

Signal-to-noise ratio (often abbreviated SNR or S/N) is a measure that compares the level of a desired signal to the level of background noise. It is defined as the ratio of signal power to the noise power. A ratio higher than 1:1 indicates more signal than noise.

Page 25: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

RF Overview Bit Error Rate

• For digital communications, there is a need for end-to-end performance

measurements.

• The measure of that performance is usually bit-error rate (BER), which quantifies

the reliability of the entire radio system from “bits in” to “bits out,” including the

electronics, antennas and signal path in between.

• On the surface, BER is a simple concept— its definition is simply:

BER = Errors/Total Number of Bits

Page 26: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

RF Overview Latency

Latency is a measure of time delay experienced in a system, ccontributors to latency include:

•Propagation: This is simply the time it takes for information to travel

between one place and another at the speed of light.

•Transmission: The medium itself introduces some delay. The size of a

packet introduces delay in a round trip since a larger packet will take longer

to receive and return than a short one.

•Processing: Each node takes time to examine and possibly change the

header in a packet.

•Computer and storage delays: Within networks at each end of the

journey, a packet may be subject to storage and hard disk access delays at

intermediate devices.

Page 27: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

RF Overview Coding Digital Data

• Digital information cannot be sent directly in the form of 0s and 1s, it must be

encoded in the form of a signal with two states.

• This transformation of binary information into a two-state signal is done in the

base band decoder.

Page 28: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

RF Overview Coding Digital Data

• To optimize transmission, the signal must be encoded to facilitate its transmission

on the physical medium. There are various encoding systems for this purpose which

can be divided into two categories:

• Two-level encoding: the signal can only take on a strictly negative or strictly

positive value (-X or +X, where X represents a value of the physical quantity

being used to transport the signal)

• Three-level encoding: the signal can take on a strictly negative, null or strictly

positive value (-X, 0 or +X)

Page 29: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

Hardware Transmitter

Voice

CommunicationNetworks

Satellite/Ground

MCC

Data/TelemetryRF

Transmitter

Video

Page 30: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

Hardware Receiver

Commands

Voice

CommunicationNetworks

Satellite/Ground

MCC

DataRF

Receiver

Video

Page 31: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

Hardware Transmitter/Receiver

Page 32: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

Hardware Transmitter/Receiver

Page 33: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

Hardware Transmitter

•Frequency(s) •Frequency stability •Frequency setting accuracy•Coherency •Input/Output impedance•RF power output •Input power•Current requirements •Temperature ranges•Cooling•Dimensions •Weight •Connector types•Form Factor•Space rated (rad hardened)•Modulation•Duty cycle

Page 34: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

Hardware Receiver

•Frequency(s)•Bandwidth •Coherency •Input/Output impedance•Sensitivity•Signal to Noise Ratio•Input power•Current requirements •Temperature ranges•Cooling•Dimensions •Weight •Connector types•Form Factor•Space rated (rad hardened)•Demodulation•Duty cycle

Page 35: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

Hardware Antenna

Page 36: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

Hardware Antenna

Page 37: Dave  Pitre Sierra Nevada Corporation( Space Exploration Systems, Louisville)

Link Budgets

• The link budget allows the designer or analyst to alter the sizing of individual

communications components and view the resulting carrier-to-noise ratio.

• The C/N needs to be above a desired threshold decibel level in order for the

signal to be usable.

• The main alterables in the link budget equation are the size of the antenna on

the spacecraft, the frequency used and the power output of the transponder used.

• Link budgets are calculated at the worst conditions possible.


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