joel handy rob schugmann jon addison
DESCRIPTION
C ONTROL S YSTEMS D ESIGN Final Presentation. Joel Handy Rob Schugmann Jon Addison. T EAM 7. S TAR S EARCH. Final Presentation Outline. Project Overview Objective Review original design Describe project construction and functional tests Discuss successes and challenges - PowerPoint PPT PresentationTRANSCRIPT
TEAM 7
Joel HandyRob SchugmannJon Addison
STAR SEARCH
CONTROL SYSTEMS DESIGN
Final Presentation
Final Presentation Outline•Project Overview
•Objective
•Review original design
•Describe project construction and functional tests
•Discuss successes and challenges
•Future Development
Final Presentation Outline
Project OverviewProject Overview
Using a telescope can be entertaining but also frustrating
Difficulties include
•Locating a celestial object
•Keeping the object within view over time
Project OverviewProject Overview Cont
These difficulties can be overcome through the design of a motorized telescope that can track a celestial object while remaining resistant to disturbances.
Original Goals
Original Goals
• Design a self-calibrating computer-positioning telescope
• Should withstand disturbances and stay centered on the desired object
•Should be easy to use while remaining relatively cheap to implement
Design Concerns & Specifications
• Speed
Point to point movement and tracking require different speeds
• Resolution
A small change in telescope position yields a large change in the field of view
Speed
Specifications for Point to Point Movement
•72°.00 / secSpecifications for Tracking Speed
•360°/23.93446743 hrs.•15°.04107000 / hr.
Speed
Resolution
Resolution is the smallest movement possible in a system
High Resolution Requirements- 0.25 degrees- Half of the field of view at medium
magnification - Increase resolution by gearing down
the system
Resolution
Resolution and Accuracy
High Resolution Requirements- 0.25 degrees- Half of the field of view at medium
magnification - Increase resolution by gearing down
the systemAccuracy
.-0.25 degrees-Any more error and objects will leave
field of view
Resolution
Project Development
•Linear Simulation
•Motor Selection
•Non-linear Simulation
•Experimental Analysis
Project Development
Linear
Simulation
Developed mathematical model of system
Used robotic parameters to obtain required torques for a given path
Linear Simulation
Torque ConstraintsTorque
Constraints
0 0.5 1 1.5 2 2.5 3 3.5-0.06
-0.04
-0.02
0
0.02
0.04
0.06
Pa
n T
orq
ue
0 0.5 1 1.5 2 2.5 3 3.5-0.3
-0.2
-0.1
0
0.1
Tilt
To
rqu
e
Motor and Gear SelectionMotor Selection
Motor (Pittman GM8724S016)•19.5:1 internal gear ratio•Max continuous torque of .29 N/m
Gears •External gear ratio of 4:1•Overall gear ratio of 80:1
RLtool
RLtoolStep Response
Time (sec)
Am
plitu
de
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.90
0.2
0.4
0.6
0.8
1
1.2
1.4From: r
To:
y
Step Response
Time (sec)
Am
plitu
de
0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8 20
0.2
0.4
0.6
0.8
1
1.2
1.4From: r
To:
y
Pan Step Response
Tilt Step Response
Non-linear w/o
Non-linear Simulation
0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8 2-0.05
0
0.05
0.1
0.15plot of desired(blue) vs actual(black) for theta1
time (s)
posi
tion
(rad
)
0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8 2-0.05
0
0.05
0.1
0.15plot of desired(blue) vs actual(black) for theta2
time (s)
posi
tion
(rad
)
Non-linear w/
Non-linear SimulationFriction Compensation
0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8 2-0.05
0
0.05
0.1
0.15plot of desired(blue) vs actual(black) for theta1
time (s)
posi
tion
(rad
)
0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8 2-0.05
0
0.05
0.1
0.15plot of desired(blue) vs actual(black) for theta2
time (s)
posi
tion
(rad
)
Testing
Procedure
Created MATLAB script file
-Automated all initialization and operation
-Automated data collection
Testing Procedure
Experimental
Analysis
Experimental AnalysisNo Trajectory Generation
0 0.5 1 1.5 2 2.5 30
0.5
1
1.5Actual Pan Position vs. Desired Pan Position
Po
sit
ion
in
Ra
dia
ns
Time in seconds
0 0.5 1 1.5 2 2.5 3-0.2
0
0.2
0.4
0.6
0.8Actual Tilt Position vs. Desired Tilt Position
Po
sit
ion
in
Ra
dia
ns
Time in seconds
Trajectory generator
Trajectory Generation
Experimental
Analysis
Experimental AnalysisTrajectory Generation
0 0.5 1 1.5 2 2.5 3-0.5
0
0.5
1
1.5Actual Pan Position vs. Desired Pan Position
Po
sit
ion
in
Ra
dia
ns
Time in seconds
0 0.5 1 1.5 2 2.5 3-0.2
0
0.2
0.4
0.6Actual Tilt Position vs. Desired Tilt Position
Po
sit
ion
in
Ra
dia
ns
Time in seconds
Slow tracking
Slow Tracking
0 50 100 150 200 250 300 350-5
0
5
10
15
20x 10
-3 Actual Pan Position vs. Desired Pan PositionP
os
itio
n i
n R
ad
ian
s
Time in seconds
0 50 100 150 200 250 300 350-5
0
5
10
15
20x 10
-3 Actual Tilt Position vs. Desired Tilt Position
Po
sit
ion
in
Ra
dia
ns
Time in seconds
Final results
Initial vs Final Specifications
Original Goals Final Results
Speed 72 deg/sec 36 deg/sec
Resolution 0.25 deg 0.325 deg
Accuracy 0.25 deg 0.57 deg
Self Positioning Yes
Withstands Disturbances Yes
Ease of Use Yes
Challenges
• Excessive Speed
-Telescope Unsafe
-Violent movements
• Trajectory Generator
-Runtime termination
-Initial run errors
Challenges
Project CostProject Cost
Components for StarSearch
Components Manufacturer Part Number Cost Quantity Total Cost
Motor Pittman GM8724S016 112.26 2 224.52
Large Gear Stock Drive A 6A61-00NF03112 19.37 2 38.74
Small Gear Stock Drive A 6A 6-25DF03106 7.4 2 14.8
Timing Belt Stock Drive A 6R 6-1150310 4.12 2 8.24
Project Cost 286.3
Compass Sensor PNI Corp Vector-2x Magnetometer 50 1 50
Inclinometer US Digital T4 70 1 70
Telescope Jason 304-T 150 1 150
Total Cost 556.3
Future
Developments
• Sensor Integration
-Greater system autonomy
• High resolution encoders
-Would allow for much greater accuracy
• Inclusion of Position data
-Allow users to target objects by name rather than coordinates
Future Developments
Questions?
Questions