UAV Telemetry - EDGEedge.rit.edu/edge/P10231/public/FinalPoster.pdf · UAV Telemetry Primary...

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UAV Telemetry Primary Objectives: *Design a wireless system that will allow for Bidirectional Communication between Airframe Control System and a ground base station. *The base station must be outfitted with a Graphical User Interface (GUI) application that will display all relevant flight data. This includes positional and diagnostic information. System Design Serial (RS-232) data read into radio Data sent to ground radio Interprets data and displays to the user Sends take Picture command to radio Command sent to radio on UAV Command given to control board. Picture taken Software Design Components Mission Statement: UAV telemetry is a member of the unmanned aerial Vehicle family of projects that is intended to create an open source, open architecture platform for aerial imaging systems. Chris Barrett (ME), Cameron Bosnic (CE), Alvaro Prieto (EE), Daron Bell (EE), Gregg Golembeski (CE), Dr. Jason Kolodziej Project Manager Software Architect Lead Engineer Power System Design Interface Manager Faculty Advisor Graphical User Interface Radio and antenna LiPo Battery Base Antenna Specification (description) Unit of Measure Marginal Value Ideal Value Project Value Size Constraint cm 17.75x17,75x17.75 15.25x15.25x15.25 15.25x15.25.7.95 Weight Constraint kg 2.27 0.5 0.715 Range m 2000 3000 2100 Refresh Rate Hz 5 10 20 Radio Throughput bps 420 1520 115200 Radio Frequency is Non-Licensed NA NA Time of Flight minutes 30 45 > 45 Radio <-> Control Interface Data Rate bps 420 1520 115200 Radio <-> PC Interface Data Rate bps 420 1520 115200 Max acceleration m/s^2 56.7 567 > 567 Results Engineering Spec vs. Final Result -Able to be carried on UAV airframe C -capable of running for the maximum expected flight time, for all expected flight conditions. -allows for bidirectional communication between the UAV’s onboard controls system and a PC on the ground -Software is open source and multiplatform -GUI displays all relevant data -GUI allows user to send take picture command System met or exceeded all of our design goals:

Transcript of UAV Telemetry - EDGEedge.rit.edu/edge/P10231/public/FinalPoster.pdf · UAV Telemetry Primary...

Page 1: UAV Telemetry - EDGEedge.rit.edu/edge/P10231/public/FinalPoster.pdf · UAV Telemetry Primary Objectives: *Design a wireless system that will allow for Bidirectional Communication

UAV Telemetry

Primary Objectives:

*Design a wireless system that will allow for Bidirectional

Communication between Airframe Control System and a ground

base station.

*The base station must be outfitted with a Graphical User

Interface (GUI) application that will display all relevant flight

data. This includes positional and diagnostic information.

System Design

Serial

(RS-232) data

read into radio

Data sent

to ground

radio

Interprets data

and displays to

the user

Sends take

Picture command

to radio

Command sent

to radio on UAV

Command given to

control board.

Picture taken

Software Design

Components

Mission Statement:

UAV telemetry is a member of the unmanned aerial Vehicle family of projects that is

intended to create an open source, open architecture platform for aerial imaging

systems.

Chris Barrett (ME), Cameron Bosnic (CE), Alvaro Prieto (EE), Daron Bell (EE), Gregg Golembeski (CE), Dr. Jason Kolodziej

Project Manager Software Architect Lead Engineer Power System Design Interface Manager Faculty Advisor

Graphical User Interface

Radio and

antenna

LiPo Battery

Base Antenna

Specification (description)Unit of

MeasureMarginal Value Ideal Value Project Value

Size Constraint cm 17.75x17,75x17.75 15.25x15.25x15.25 15.25x15.25.7.95

Weight Constraint kg 2.27 0.5 0.715

Range m 2000 3000 2100

Refresh Rate Hz 5 10 20

Radio Throughput bps 420 1520 115200

Radio Frequency is Non-Licensed NA NA

Time of Flight minutes 30 45 > 45

Radio <-> Control Interface Data Rate bps 420 1520 115200

Radio <-> PC Interface Data Rate bps 420 1520 115200

Max acceleration m/s^2 56.7 567 > 567

Results

Engineering Spec vs. Final Result

-Able to be carried on UAV airframe C

-capable of running for the maximum expected flight time,

for all expected flight conditions.

-allows for bidirectional communication between

the UAV’s onboard controls system and a PC on the ground

-Software is open source and multiplatform

-GUI displays all relevant data

-GUI allows user to send take picture command

System met or exceeded all of our design goals: