1 jet propulsion laboratory jpl flight team adam nikolic josh ruggiero bob hoffman dusty terrill
TRANSCRIPT
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1
Jet Propulsion Laboratory
JPL Flight Team
Adam Nikolic
Josh Ruggiero
Bob Hoffman
Dusty Terrill
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Jet Propulsion Laboratory
Completed so far
• Schedule
• Initial research
• Architecture Description
• System requirement document
• Created CVS Server
• System design
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Jet Propulsion Laboratory
Schedule - Done
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Jet Propulsion Laboratory
Schedule - Not Done
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Jet Propulsion Laboratory
Initial Research
• Standards and requirements
– CCDCS for communication
– IEEE 1471 for architecture description
– VML2
• Basics of space flight
– Satellite components and configuration
– Orbit patterns and flight mechanics
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Jet Propulsion Laboratory
Architecture Description
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Jet Propulsion Laboratory
System Requirement Document
• Flight Requirements:
• The flight system shall track and analyze changes in terrestrial features
• The flight system shall use a 5-10m resolution
• The flight system shall moderate cost
• The flight system shall use 1500 x 1500 picture resolution
• The flight system shall be able to take visible and infrared images
• The flight system shall accept targets from Mission Control
• The flight system shall create flight path from Mission Control targets
• The flight system shall send health/status information to Mission Control
• The flight system shall use JPEG image format
• The flight system shall send an image to Mission Control once it has been taken image
• The flight system shall send the following information as health/status information:
• Fuel (Kg/g), Velocity (km/s), Altitude (km), Battery Power (mW), Power Consumption (mW/H), number of reads, number of writes, how much free memory (GBytes), and position (spherical coordinates).
• The flight system shall accept image request from Mission Control
• The flight system shall accept a request for a TIFF or BMP image from Mission Control and then send the specified image format.
• The flight system shall minimize power usage
• The flight system shall design a propulsion system
• The flight system shall design a navigation system
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Jet Propulsion Laboratory
System design
• Memory – 2 separate memory modules (assuming 1 million writes per module)
• Maximum bmp memory – 2MB
• Status info/data
– Fuel (Kg/g) – (Capacity 26Kg) – 15 bits
– Velocity (m/s) – (Max around 7600 m/s) - 13 bits
– Altitude (km) – (900km max height) – 10 bits
– Battery Power (mW) – (850W x 2 batteries) – 11 bits
– Power Consumption (mW/H) – (max can use is 1700) – 11 bits
– number of reads – (3 million reads) – 22 bits
– number of writes – (1 million writes x 2) – 40 bits
– Position (spherical coordinates) – (max 360°) – 9 bits
– ground control commands – (Location to move to) – 24 bits
• Power – Power consumption info
• Four deployable, fixed solar panels and one body-mounted panel contain 3.4 m2 of solar cells and provide 230 W/hr of orbital average power
• 2 batteries (.5 m3) each provide 850W/hr power, takes 3 hours to charge.
• Consumptions uses:
• -Antenna: 25W per transmission
• -CPU: 50W
• -Thrusters: 100W per course correction
• -Camera: 30W
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Jet Propulsion Laboratory
Left to do
This Semester
Finish overall system design
Start working on UML diagrams
Use cases and class diagrams
Start making schedule for next semester
Next Semester
Code
Code
Code