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Image Processing of Remotely Sensed Data
ImAP RSD Image Processing of Remotely Sensed Data
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Team Members Advisor: Dr. Basart
Client: Space Systems Control Laboratory (SSCL) EE 491: Matt Clausman, Jesse Griggs, Christina McCourt, Andy Schulte, Shobhit Vaish EE 492: Usman Aurakzai, Ali Khan, Chia- Yuan Chang
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Problem Statement General Problem Statement: General ImAP Solution
There is no efficient, low cost, and easy to use method of aerially monitoring crop health and yield General ImAP Solution Suspend a payload from a high-altitude balloon that is capable of taking photos and storing the data for analysis.
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Current Methods Balloon 9000 – 20000+ feet Aircraft 500 – 9000 feet
Radiometer 10 feet Soybean
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System Overview
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Current Semester’s Focus
Horizon Detection System (HDS) Determine the spatial orientation of the payload for effective aiming of the camera system Pitch Roll
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Possible HDS Solutions
Image Processing Concept: Take pictures on each side of the payload Use image processing to detect horizon and position camera system correctly Benefits: Greater accuracy Drawbacks: Much higher cost Measurements affected by rough terrain, clouds, and other obstructions More processing power
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Possible HDS Solutions (continued)
Thermopiles Concept: Measure temperature differential between the earth and sky Use output voltage as feedback in order to position camera system correctly Benefits: Cheap implementation Less complex Reality check Drawbacks: Less accurate
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HDS System Diagram
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Market Research Horizon detection using imaging
More advanced image processing algorithms Supercomputers to process data Horizon detection using thermopiles Lower altitude using a plane Different control scheme
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HDS Functional Requirements
HDS shall provide roll and pitch accurate to 3 degrees when operated between 20,000 and 30,000 ft. HDS shall operate during the daytime hours with a sky of less than 30% cloud cover. HDS shall receive power from a 11.1 V nominal lithium-ion battery. HDS shall function for a minimum of 3 hours using a 4 Amp-hour battery pack.
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HDS Non-functional Requirements
The weight of the payload shall be less than 4 lbs. The payload shall occupy less than 1 cubic foot
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Project Plan Work breakdown Budget Thermopiles: Jesse
FPGA and Image Processing: Matt MATLAB Image Processing: Andy, Shobhit Technical manual, Gantt chart, and other documentation: Christina Budget Thermopile system: $100 Image Processing system: $300
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Deliverables HDS Documentation Thermopile system
Design Prototype Proof of concept Image processing system Documentation Operational manual
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