a 3u cubesat prototype to measure solar irradiance€¦ · radiance is a 3u cubesat-style payload...
TRANSCRIPT
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Team: Brandon Antoniak, Russell Bjella, Katelyn Dudley, Alec Fiala, Jennifer Kampmeier, Jeremy Muesing, David Varley, Lance Walton, James PavekAdvisor: Dr. Robert A. Marshall Customer: Dr. Scott Sewell, HAO
A 3U CubeSat Prototype to Measure Solar Irradiance
Spring Final Review, May 4, 2017
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Outline
2
• JennyPurpose and Objectives
• LanceDesign Description
• KatieTest Overview
• Brandon, KatieTest Results
• AlecSystems Engineering
• JennyProject Management
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15%
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Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Project Motivation
3
Solar irradiance data is plentiful, but…
The record has gapsDatasets vary between different instrumentsFull-scale space missions are costly and time-consuming
Are these variations real?How does it inform climate
science?
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Project Future
4Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Project Description
5Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
• Mission Statement
• Project Statement
RADIANCE is a 3U CubeSat-style payload that will collect solar irradiance data, images, attitude information, and ambient atmospheric data during a 2-week circumpolar high-altitude balloon flight.
The mission will launch from Antarctica between November 2017 and February 2018.
RADIANCE will design, build, test, and deliver a 3U CubeSat-style payload to collect solar irradiance data, images, attitude information, and ambient atmospheric data on a high-altitude balloon flight.
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HiWind Gondola & Flight
6
Mission:Ground: 8 hoursAscent: 2 hoursFlight: 2 weeksDescent: 1 hour
4.5 m wide5.0 m tall2000 kgRADIANCE
mounting location
Gondola:
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Concept of Operations
7Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Project-Level ConOps
8Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Levels of Success
9
System Level Met Details
Instr. 3
Take solar irradiance measurements at better than 1.5nm resolution covering 250-1000nm
Capture 1 photo/min of the Sun for full flight
Provide calibration of the instrument
C&DH 3Record solar irradiance, attitude, environmental, and housekeeping data on a durable data storage device with sufficient capacity
Thermal 1 All systems survive ascent and descent, all systems operate during the cruise
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Levels of Success
10
System Level Met Details
ADS2 Determine and record attitude to 1 arcminute of accuracy
relative to the sun vector
1 Determine and record attitude to 1° of accuracy relative to the sun vector
EPDS 1 Package operates on HiWind power supply
Structure 1
Structure must be within 10cm x 10cm x 32cm
Data is recoverable after up to 5 Gs on landing
Structure can be affixed to HiWind
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Design Overview
11Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Functional Requirements
12
RADIANCE shall…
FR1: Take solar irradiance measurements.FR2: Survive the environmental conditions of a high-altitude
balloon flight up to 40 km.FR3: Return data.FR4: Determine its attitude.FR5: Interface with the HiWind Gondola.FR6: Capture images of the Sun in the visible spectrum.
The project deliverables shall include a Path-to-Space report.
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Executive Summary
13
Parameter Overall Values Req.Dimensions 31.81 cm x 15.1 cm x 10 cm DR5.1Mass 3.0 ± 0.05 kg —Power 3.2 to 19.6 W usage, ~3.2 W average at cruise DR5.4Thermal -3 to 60°C internally, spot-heated in critical places FR2
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Complete Assembly
14Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
15Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
16
Internal structure attached to external struts with screwsAttachment points to HiWind
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
17Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
18Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
19Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
20Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
21Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
22
Photodiode array and circuit board for attitude determination4 photodiodes offset at 45° to determine off-sun angle to ≤ 1°
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
23Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
24
Camera assembly, including:
Raspberry Pi CameraAdjustable focus lens and mountingDouble-layer neutral density filter
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
25Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
26
Spectrometer and fiber optic cable from Avantes
Req. SolutionResolution ≤ 1.5 nm 1.4 nmWavelength 250-1000 nm 200-1100 nmCost ~$3000 $2946Size Must fit 90x68x20 mmPower < 3W 1.25 WInterface RPi required RPi capable
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
27Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
28Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
29Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
30
Raspberry Pi microcontroller
Req. SolutionSize Must fit 85x56x17 mmCost < $100 $36Versatility High COTSInterface RPi needed RPi capable
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
31
Three USB storage devices:
1 single-level cell (SLC) drive2 multi-level cell (MLC) drives
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
32Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
33Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
34Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
35
Two Lithium Ion batteries
Needed to power active thermal system
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
36
Custom power board for control and distribution
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
37
External sensors (temperature, relative humidity) for atmospheric measurementsInternal temperature sensors for active thermal monitoring
HK SensorsENV Sensors
(On Back)
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
38
Polyurethane foam insulationThin film resistive heaters for active thermal control
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
39Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
40Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Overview
41Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Functional Block Diagram
42
Header
DC-DC
Batteries
DC-DC
HiWind
SLC Drive
MLC Drive
MLC Drive
USB
Power
Header CSI
Heaters
DataPower
Humidity
Ext. Temp.
HK Temp.
ADS
Camera
Spectrometer
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Changes Since TRR
43
Power boardUpdated wiring during integrationChanged some resistor values to handle more current
Camera FOV reduced to ~1.57° from original 6.32°Timing loop has changedNeutral density filter values adjusted from qualitative assessment of camera images
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Critical Project Elements
44
CPE Justification FR
Thermal Control All components must meet thermal requirements 2
Power Power board design is complex 5
Software Efficient software design is critical to mission success 3
Camera, Lens Challenging assembly to ensure in-focus images 6
Attitude Determination
Complex design, small parts, challenging hardware/software interface 4
No changes since MSR or TRR.
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Test Overview
45Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Component Testing
46Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
Integration Testing
SubsystemTesting
ComponentTesting
Purpose:Verify components turn onVerify measurements are reasonableCompare with expected performance from
data sheetInvestigate need for calibration (and
perform calibration)
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Component Testing
47Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
Integration Testing
SubsystemTesting
ComponentTesting
Purpose:Verify and integrate operation of
subsystemsVerify interaction between software and
hardwareValidate CAD model and attitude
determination model
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Component Testing
48Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
Integration Testing
SubsystemTesting
ComponentTesting
Purpose:Verify and demonstrate integrated
operation of full systemValidate SolidWorks thermal, C&DH
storage capacity, and timing models
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Attitude Test Overview
49Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
Test: Verify resolution of attitude determination measurements
Why? FR4 requires ≤ 1° accuracy
How?
1. Mount system to telescope
2. Track the sun3. Turn off tracking software4. Allow ADS to measure
drift angle
Resource Sommers Bausch Observatory
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TVAC Test Overview
50Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
Test: Validate thermal model during cruise conditions
Why?System must survive the environmental conditions of flight.
How?
1. Allow chamber to reach desired temperature
2. Power on system3. Pump down to ~200 Pa4. Allow system to reach
thermal equilibrium
Resource TVAC Chamber at HAO
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Environmental Chamber
51Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
Test: Validate thermal model during ascent conditions
Why?Want the system to operate during the environmental conditions of ascent.
How?
1. System rests for one hour at pre-launch ground temperature (-10°C)
2. Expose system thermal ascent profile
3. Record voltage and temperature data
Resource Environmental chamber in Bioastronautics Lab (CU)
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Benchtop Test Overview
52Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
Test: Validate benchtop thermal model
Why?Gives confidence to other thermal models not tested due to TVAC issues.
How?
1. Assemble system with side panels
2. Power on system3. Allow to run for 2 hours4. Record temperature and
voltage data
Resource Trudy Schwartz’s Lab
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Test Results: Component Tests
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Spectrometer Calibration
54
Avantes Deuterium light sourceCalibration stored on spectrometer
FR 1: The system shall measure solar irradiance.
DR 1.1.2: The spectrometer shall be calibrated
Instr. LoS: 3
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Emissive Coating Verification
55
Thermal camera usedGoal is
Actual Emissivity
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Camera Images
56
FR 3: The system shall image the sun.
Instr. LoS: 3
Camera FOVExpected Actual Req.
1.21° ~1.57° < 10°
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
0.5°
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Preliminary Photodiode Array
57
First photodiode tests in sun gave photocurrents on order of 2.5 mAChanged transimpedance amp to 1 kΩ instead of 5 kΩfeedback resistance
Prevent saturating the ADCs
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Attitude Determination Test
58
FR 4: The system shall determine its attitude.
DR 4.1: The off-sun angle shall be determined to better than one degree of accuracy.
Attitude LoS: TBD
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Attitude Determination: Model
59
1 arcminute of movement occurs 4.03 seconds after turning off the sidereal tracker
Solar angle rate = 0.2482 ± 0.0003 arcmin/sec(over 3 minute test)
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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ADS Noise Requirement
60
Tested photodiode response with handheld LED light source
Shaky handsLED not as powerful at red wavelengths as the sun
Noise is ~2.6 mVRequired for 1° accuracy: < 32.6 mVRequired for 1’ accuracy: < 0.5 mV
Noise is ~2.6 mV
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Attitude Determination: Expected Results
61
Full test occurred week of April 24th
Results discussed during presentation
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Test Results: Integration
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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TVAC: Model
63
SolidWorks transient simulationAssume convection coefficient = 0 for vacuumActual radiative coating emissivity from IR analysis
Property ValueConvection Coefficient 0Radiation Temperature 18°CConduction Temperature 18°CRadiative Coating Emissivity 0.80
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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TVAC: Spectrometer Analog
64
Started simultaneously with RADIANCE onboard systemsCaptured data through entire testData questionable due to proximity to heater
Uncertainty: ±0.06°C
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
Repressurized Chamber
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TVAC: Results
65
Due to software bug, error handling failed→ 25 minutes of data
Uncertainties:Raspberry Pi: ± 2°CBatteries: ± 0.06°C
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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TVAC: Conclusions
66
FR2: The system shall survive the environmental conditions of flight
DR 2.4 The system shall survive the pressure range from 200 Pa to 100 kPa
Thermal LoS: 1
Transient solutions for components actively producing heat are questionableModels for components not actively producing heat are supported by current test dataLonger tests are needed to validatetransient models. Current test data encouragesconfidence in transient models
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Benchtop Thermal: Model
67
Radiation and convection temperatures = 25°CActual radiative coating emissivity from IR analysis 𝜖 = .80
SolidWorks steady state simulationConvection coefficient = 4.4
From basic principles MATLAB model
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
Temp (°C)
54525149474644424139383634
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Benchtop Thermal: Results
68
Error handling bug resolved
Uncertainties:Raspberry Pi: ± 2°CBatteries: ± 0.06°C
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Benchtop Thermal: Results
69
FR2: The system shall survive the environmental conditions of flight.
Thermal LoS: 1
Models for atmospheric steady state are supported by current test resultsRaspberry Pi likely will always run hotter than model due to CPU proximity to temperature sensorTesting at vacuum is needed to validate vacuum steady state models.Current test data encouragesconfidence in transient models
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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C&DH Timing: Model
70
Total TimeTime: 0.491 s
250ms 52ms 100ms 46ms
8ms5ms
30ms
ISO 400 Camera Integration Time (Variable)Camera
Read
Spectrometer Integration Time
(Variable)Spec Read
Processing Time
Camera Write
Spec Write
Pi Camera
Spectrometer
Raspberry Pi MLC
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
SLC
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C&DH Timing: Results
71
Item TimeSpectrometer Integration Time 1.05 msSpectrometer Read Time 5 msCamera Integration Time 250 msCamera Read Time 950 ms1Wire Internal Temperature Sensors 2.5 sRemaining Sensors <1 msWrite to Storage 1 ms
Total Time (with Camera)Time: 3.75 s ± 30 ms
Total Time (without Camera)Time: 2.6 s ± 30 ms
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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C&DH Timing: Conclusions
72
FR 3: The system shall return data.DR 3.1.1 Science data shall be recorded once per minute.
DR 3.1.2 Science instrument measurements shall be recorded within 2 seconds.
DR 3.1.3 Camera images shall be recorded once per minute.
Data LoS: 3
Item Req. Model ActualScience Data Cadence 60 s 1 s 2.6 s
Science Data Lag 2 s 13 ms 1 ms
Camera Image Cadence 60 s 60 s 60 s
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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C&DH Capacity
73
Measurement Model Total Actual TotalSpectrometer 9.25 GB 3.63 GBExternal temperature 4.6 MB 1.8 MBInternal temperature 27.7 MB 5.3 MBHumidity 4.6 MB 1.8 MBPhotodiode (x4) 36.9 MB 7.1 MBSun angle 4.6 MB 0 BTotal 9.4 GB 3.65 GB
Measurement Model Total Actual TotalCamera images 17.7 GB 3.63 GBOther Data 9.4 GB 3.65 GBTotal 27.1 GB 7.28 GB
SLC Flash Drive 14.9 GB Capacity
Modeled Margin: 37%Actual Margin: 76%
MLC Flash Drive (2)59.6 GB Capacity
Modeled Margin: 55%Actual Margin: 88%
Overall mission capacity uncertainty:
±10.7%
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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C&DH Capacity: Conclusions
74
FR 3: The system shall return data.DR 3.1: The data shall be recorded. Data LoS: 3
0 10 20 30 40 50 60 70
MLC Modeled
MLC Actual
SLC Modeled
SLC Actual
Data Volume in GB
Spectrometer ADS Small Sensors Images Margin
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Power Budget: Model & Results
75
Component Modeled Power Draw
Raspberry Pi 4.25 WSpectrometer 1.25 WCamera 0.7 WSmall Sensors 0.1 WFlash Drives 1.4 WTotal (Cruise) 7.7 WHiWind Power 15 W
Measured Total Power Draw:3.2 ± 0.5 W
Power LoS: 1
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Systems Engineering
76Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Systems Engineering
77
System Validation
System Verification
Subsystem Verification
Component Testing
Concept of Operations
Requirements
High Level Design
Detailed Design
Manufacturing
PDD
CDD
PDR
CDR
MSR
Delivery
TRR
SFR
Integration
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Component Test Mapping
78
Component Testing
Detailed Design
Relate individual components to CDR level design and sub requirementsVerify functionality of aspects such as ENV and HK sensors
Lessons Learned:“Components” still require integrationEasy for issues to push schedule
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Subsystem Integration
79
Subsystem Verification
High Level Design
Lessons Learned:Wire design and harnessing is crucial
Test functionality of system subsetsVerify PDR level design aspects
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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System Integration
80
System VerificationRequirements
Requirement CompletionSolar irradiance 4/4 VerifiedEnvironmental conditions
3/6 Verified
Data 2/2 VerifiedAttitude 0/2 VerifiedInterface 6/6 VerifiedImaging 3/3 Verified
Lessons Learned:Most issues occurred during this phaseBudget time and money to fix issues that come up
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Requirements: Solar Irradiance
81
Verified
To be verified:
1.1: Spectrometer derived requirements250 to 1000 nm, < 1.5 nm resolution, calibrated
1.2: Environmental sensor derived requirementsMeasure temperature and humidity once per minute
None!
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Requirements: Environment
82
Verified
To be verified:
2.4: Humidity of 5% to 90%2.5: Pressure of 0.20 kPa to 100 kPa2.6: Resist radiation effects
2.1: Ground temperatures2.2: Ascent temperatures2.3: Cruise temperatures
To be verified in environmental testing by HAO
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Requirements: Data
83
Verified
To be verified:
3.1: Data storage rate of once per minute and derived requirements3.2: Data storage survives landing
None!
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Requirements: Attitude
84
Verified
To be verified:
4.1: Accuracy within one arcminute4.2: Data storage rate of once per minute
TBD
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
To be verified in SBO testing
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Requirements: Interface
85
Verified
To be verified:
None!
5.1: Dimensions of 32 cm x 10 cm x 10 cm5.2: Sun facing plate is the 10 cm x 10 cm5.3: Power interface and derived requirements
15 W at 28-33 V5.4: ICD compliance
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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ICD
86
Created ICD for HiWind/RADIANCE IntegrationDefines structural, electrical interfacesDefines interface associated risks
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Requirements: Imaging
87
Verified
To be verified:
None!
6.1: Image storage on drives5.2: Field of view of 5° ± 3°5.3: Image cadence of once per minute
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Projects Risk Matrix – Post CDR
88
Likelihood
Consequences
Risks easily mitigated
1 FR Failed 2-3 FRs Failed
3-4 FRs Failed
5-6 FRs Failed
Certain 1 5
Likely 4
Moderate 1 3
Unlikely 4 2
Rare 4 1 1 1
1 2 3 4 5
1
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Risk Status
89
Element Value Test Current StatusOverheating 5 TVAC Thermal Model ValidatedFrost on optics 5 Acceptable RiskHeater failure 3 TVAC No recorded failureDrive hardware failure 4 Acceptable RiskTemporary power failure 3 Flatsat Mitigated with batteries in
Flatsat testingSoftware data write failure 2 FlatsatBit flip 2 Acceptable riskDrive connection failure 2 Acceptable riskCamera Oversaturation 2 SBO Image takenPi Software failure 1 Flatsat Pi restarts as expected
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Risk Summary
90
Additional Risks
Changes to risks
Improper power cycling may cause SD card corruptionFew software risks identified by CDR (mitigated during testing)Scheduling risks
Increased risk of heater failure in vacuumQB50 team encountered issues, including recommended heater in path to space
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Project Management
91Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Management Approach
92
Proactive efforts to build a positive, supportive team environment
Encouraged discussion from the start to work towards solutionsEvery team member’s contribution is valuable and their perspective is valid
“Leadership Through Service”
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Success and Challenges
93
Success: We all still like each otherSuccess: Peer ReviewsChallenge: Time management with
other obligations (work, courses, etc.)Needs of the project vs. needs of the team
Sometimes it felt like…
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Success and Challenges
94Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Lessons Learned
95
Diverse project led to scattered focus at times à important to be aware of this
80/20 ruleBalance between when to go for the extra 20% and when to let it go
Need to balance burn-out with productivity
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Individual Hours Worked
96Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Team Hours Worked
97Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Hours per Person per Week
98
050
100150200250300350400
9/9
9/16
9/
23
9/30
10
/7
10/1
4 10
/21
10/2
8 11
/4
11/1
1 11
/18
11/2
5 12
/2
12/9
1/
20
1/27
2/
3 2/
10
2/17
2/
24
3/3
3/10
3/
17
3/24
3/
31
4/7
4/14
4/
21
Hours per Person per Week
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Budget
99
Subsystem ProjectedCost Procured To be
Procured Margin (%) Effect on Budget
C&DH $ 167 $ 149 — — +$ 18Sensors $ 203 $ 127 — — +$ 76Instrumentation $2988 $3052 — — –$ 64Power $ 662 $ 615 $ 39 $ 8 –$ 50PM $ 84 $ 49 — — +$ 35Structure $ 418 $ 223 $ 4 $ 6 +$185Testing $ 250 $ 77 $ 16 $ 157 —Thermal $ 66 $ 36 — — +$ 30TOTAL $4613 $4327 $ 59 $ 171 (290%) +$230
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Equivalent Industry Cost
100
Estimate Cost
CDR Estimate $4920MSR Estimate $4634TRR Estimate $4613SFR Estimate $4613
Billable Item Cost
5056 Hours $157,997Materials $ 5,000Overhead 200%“Industry Cost” $478,991
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Acknowledgements
101
Scott Sewell and Phil Oakley, HAO/NCARTrudy Schwartz, CU BoulderBobby Hodgkinson, CU BoulderFabio Mezzalira, Sommers Bausch ObservatoryAndrew Dahir and Nicholas Rainville, QB50James Mason, MinXSSSteve McGuire, CU Boulder
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Thank you!We welcome your questions!
102Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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BACKUP SLIDES
103
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Manufacturing Process
104
Conventional manufacturing techniquesOnly minor manufacturing issues3D printed parts required several iterations
10 cm
30 cm 15.1 cm
3.8 cm
3.8 cm
2.6 cm
2 cm
2.2 cm
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Structural Design Motivations
105
Previous flight data: speed is 5.44 m/s at landingEquipped with parachute and crush pads Data only taken every ~30 seconds à must infer landing force using Δ in momentum
R3.2: Data storage shall survive landing
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Structural Design
106
From previous data:
Estimated crash duration:
Fundamental equations:
Landing Impact3.30 Gs
Flash Drive Rating1500 Gs
Duration determined based on height of crush pads and speed
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Camera
107
Using flux and size of the sun on the image sensor, find total power:
Known parameters:
Field of View Calculation
LensMountCamera board
Neutral Density Filter Calculation
Choose filter with 96.875% attenuation
(OD of 1.5)
Result:
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Humidity Sensor Calibration
108
Systematic bias of ~36%Straightforward adjustment in software
DR 1.2 The system shall take environmental
measurements.
Rel
ativ
e H
umid
ity [%
]
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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Battery Capacity
109
Battery trending between the two cells is in familyLower than published data, but within starting tolerance
of 3.6 to 4.2 V; system noise is approximately 17 mV
Purpose & Objectives
Design Overview
Test Overview
Test Results
Project Management
Systems Engineering
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C&DH Capacity: Model
110
Measurement Data Point Size Frequency TotalSpectrometer 8.2 kB 1 s 9.25 GBExternal temperature 4 B 1 s 4.6 MB
Internal temps (x6) 24 B 1 s 27.7 MBHumidity 4 B 1 s 4.6 MBPhotodiode (x4) 32 B 1 s 36.9 MBSun angle 4 B 1 s 4.6 MBTotal 8.3 kB -- 9.4 GBMeasurement Data Point Size Frequency TotalCamera images 920 kB 60 s 17.7 GBOther Data 8.3 kB 1 s 9.4 GBTotal 936.5 kB -- 27.1 GB
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C&DH Capacity: Results
111
Measurement Data Point Size Frequency Total
Spectrometer 8.19 kB 2.602 s 3.63 GBExternal temperature 4 B 2.602 s 1.8 MB
Internal temps (x3) 12 B 2.602 s 5.3 MBHumidity 4 B 2.602 s 1.8 MBPhotodiode (x4) 16 B 2.602 s 7.1 MBSun angle 0 B 2.602 s 0 BTotal 8.24 kB -- 3.65 GBMeasurement Data Point Size Frequency TotalCamera images 152 kB 60 s 3.63 GBOther Data 8.24 kB 2.602 s 3.65 GBTotal 160.24 kB -- 7.28 GB
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Light Attenuation
112
Test mA
Current without ND Filter 10.07
Current with ND Filter (Expected) 1.007
Current with ND Filter (Actual) 0.97
Error = 3.6%