spacecraft avionics...spacecraft avionics enae 483/788d - principles of space systems design u n i v...
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Spacecraft Avionics
• Lecture #26 – November 21, 2019 • Avionics overview • Sensors and actuators • Shuttle systems • Constellation systems • Sensors
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© 2019 David L. Akin - All rights reserved http://spacecraft.ssl.umd.edu
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Avionics Functions
from J. F. Hanaway and R. W. Morehead, Space Shuttle Avionics Systems - NASA SP-504, 1989
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Spacecraft Data Processing System
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from Pisacane, Fundamentals of Space Systems, 2nd ed., Oxford Univ. Press, 2005
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Shuttle Data Bus Architecture
from J. F. Hanaway and R. W. Morehead, Space Shuttle Avionics Systems - NASA SP-504, 1989
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Displays and Controls Block Diagram
from J. F. Hanaway and R. W. Morehead, Space Shuttle Avionics Systems - NASA SP-504, 1989
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Communications Block Diagram
from J. F. Hanaway and R. W. Morehead, Space Shuttle Avionics Systems - NASA SP-504, 1989
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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On-Orbit Communications Links
from J. F. Hanaway and R. W. Morehead, Space Shuttle Avionics Systems - NASA SP-504, 1989
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Shuttle Antenna Locations
from J. F. Hanaway and R. W. Morehead, Space Shuttle Avionics Systems - NASA SP-504, 1989
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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S-Band Network Equipment
from J. F. Hanaway and R. W. Morehead, Space Shuttle Avionics Systems - NASA SP-504, 1989
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Ku-Band Radar and Communications
from J. F. Hanaway and R. W. Morehead, Space Shuttle Avionics Systems - NASA SP-504, 1989
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Shuttle Baseline Systems Architecture
from J. F. Hanaway and R. W. Morehead, Space Shuttle Avionics Systems - NASA SP-504, 1989
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Shuttle Avionics Installations
from J. F. Hanaway and R. W. Morehead, Space Shuttle Avionics Systems - NASA SP-504, 1989
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Software Architecture
from J. F. Hanaway and R. W. Morehead, Space Shuttle Avionics Systems - NASA SP-504, 1989
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Navigation, Guidance, and Control Elements
from J. F. Hanaway and R. W. Morehead, Space Shuttle Avionics Systems - NASA SP-504, 1989
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Reaction Control System Architecture
from J. F. Hanaway and R. W. Morehead, Space Shuttle Avionics Systems - NASA SP-504, 1989
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Crew Audio System
from J. F. Hanaway and R. W. Morehead, Space Shuttle Avionics Systems - NASA SP-504, 1989
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Electrical Power Distribution Bus (1 of 3)
from J. F. Hanaway and R. W. Morehead, Space Shuttle Avionics Systems - NASA SP-504, 1989
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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CEV Avionics Architecture
• Command and Data Handling (C&DH) • Displays and Control (D&C) • Communications and Tracking (C&T) • Instrumentation wiring • Flight software
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
So How Do You Do “Avionics”?• Create specifications
– Sensor list (type, location, number, criticality) – Networking strategy – Estimate of processing throughput
• Complexity of controlling equations • Required cycle times
– Communications bandwidth
• Select critical components – Data management units – Redundancy strategies – Communications frequencies
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Avionics Design (continued)
• System block diagrams • Interface control documentation • Power and thermal budgets • Crew interfaces (controls and displays) • Failure modes and effects analysis • Probabilistic risk assessment
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Sensing Definitions
• Resolution • Accuracy • Precision/Repeatability
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Resolution
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Some Notes on Data and Noise
• Noise is inherent in all data – Sampling errors – Sensor error – Interference and cross-talk
• For zero-mean noise, – Integration reduces noise – Differentiation increases noise
• Use the appropriate sensor for the measurement – Don’t try to differentiate position for velocity,
velocity for acceleration
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Shannon Sampling Limit
• For discrete measurements, can’t reconstruct frequency greater than 1/2 the sampling rate
• Discretization error creates aliasing errors (frequencies that aren’t really there) – Signal frequency ƒsignal – Sampling frequency ƒsample – Alias frequencies ƒsample ± ƒsignal
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Analog and Digital Data
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Analog and Digital Data with Noise
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Some Notes on Analog Sensors• Analog sensors encode information in voltage
(or sometimes current) • Intrinsically can have infinite precision on signal
measurement • Practically limited by noise on line, precision of
analog/digital encoder • Differentiation between high level (signal
variance~volts) and low level (signal variance~millivolts) sensors
• Advice: never do analog what you can do digitally
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Proprioceptive Sensors
• Measure internal state of system in the environment
• Rotary position • Linear position • Velocity • Accelerations • Temperature
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Proprioceptive Sensors
• Position and velocity (encoders, etc.) • Location (GPS) • Attitude
– Inertial measurement units (IMU) – Accelerometers – Horizon sensors
• Force sensors
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Representative Sensors
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Absolute Encoders
• Measure absolute rotational position of shaft • Should produce unambiguous position even
immediately following power-up • Rovers typically require continuous rotation
sensors • General rule of thumb: never do in analog what
you can do digitally (due to noise, RF interference, cross-talk, etc.)
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Rotary Binary Encoder
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Binary Absolute Position Encoders
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Gray Code Absolute Position Encoders
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Absolute Encoder Gray Codes
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Optical Absolute Encoders
• Advantages – No contact (low/no friction) – Absolute angular position to limits of resolution
• 8 bit = 256 positions/rev = 1.4° resolution • 16 bit = 65,536 positions = 0.0055° resolution
• Require decoding (look-up table) of Gray codes • Number of wires ~ number of bits plus two
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Magnetic Absolute Encoders
• Advantages – No contact (low/no friction) – Absolute angular position to limits of resolution
• 8 bit = 256 positions/rev = 1.4° resolution • 16 bit = 65,536 positions = 0.0055° resolution
– Robust to launch loads
• Require decoding (frequently on chip) • Choice of output reading formats (analog,
serial, parallel)
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Incremental Encoders
• Measure change in position, not position directly
• Have to be integrated to produce position • Require absolute reference (index pulse) to
calibrate • Can be used to calculate velocities • Generally optical or magnetic (no contact)
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Incremental Encoder Principles
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Quadrature Incremental Encoder
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Incremental Encoder Interpretation• Position
– Count up/down based on quadrature (finite state machine)
– Resolution based on location, gearing, speed • 256 pulse encoder (1024 with quadrature) • Output side – 0.35 deg • Input side 160:1 gearing – 0.0022 deg = 7.9 arcsec
• Velocity – Pulses/time period
• High precision for large number of pulses (high speed) • 90 deg/sec, input side – 41 pulses/msec (2.5% error)
– Time/counts • High precision for long time between pulses (low speed) • 1 deg/sec, output side – 350 msec/pulse
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Velocity Measurement
• Number of bits/unit time – High precision for rapid rotation – Low resolution at slow rotation – For n bit encoder reading k bits/interval
• Amount of time between encoder bits – High precision for rapid rotation – Low resolution for slow rotation
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! =k
2n2⇡
�tCLKhradsec
i
! =1
2n2⇡
�tpulseshradsec
i
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Exterioceptive Sensors
• Measure parameters external to system • Pressure • Forces and torques • Vision • Proximity • Active ranging
– Radar – Sonar – Lidar
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Exteroceptive Sensors
• Vision sensors – Monocular – Stereo/multiple cameras – Structured lighting
• Ranging systems – Laser line scanners – LIDAR – Flash LIDAR – RADAR – SONAR
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Switches
• Used to indicate immediate proximity, contact – End of travel/hard stops – Contact with environment
• Technologies – Mechanical switches – Reed (magnetic) switches – Hall effect sensors
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Computer Vision Cameras
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Scanning Laser Rangefinder
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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LIDAR Types
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
SpaceX DragonEye Flash LIDAR
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Flash LiDAR
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Interoceptive Sensors
• Electrical (voltage, current) • Temperature • Battery charge state • Stress/strain (strain gauges) • Sound
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Strain Gauges
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Strain Gauge with “Dummy” Gauge
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
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Wheatstone Bridge
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Temperature Sensors
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• Contact – Thermistors – Resistant Temperature Detectors (RTDs) – Thermocouples
• Non-contact – Infrared – Thermal generators (thermopiles)
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Spacecraft Avionics ENAE 483/788D - Principles of Space Systems Design
U N I V E R S I T Y O FMARYLAND
Sensor Guidelines for Flight Systems
• Instrument every flight-critical activity • Provide sufficient sensor redundancy to
differentiate between sensor failure and system failure – Redundant sensors – Reinforcing sensors
• Interrogate sensors well beyond Shannon’s limit (cannot reconstruct data without at least two samples/cycle)
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