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Precision Navigation for Small Unattended Aerial Vehicles

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Precision Navigation for Small Unattended Aerial Vehicles ... College of Engineering Faculty. Embry-Riddle Aeronautical University. McNair Scholars Program ... – PowerPoint PPT presentation

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Title: Precision Navigation for Small Unattended Aerial Vehicles


1
Precision Navigation for Small Unattended Aerial
Vehicles
McNair Scholars Program
  • Drake Miller
  • Faculty Mentor Dr. Gary Gear

2
Overview
  • Research Thrust
  • Unattended Aerial Vehicle (UAV) Background
  • Full Scope of Research
  • Future Work

3
Research Thrust
  • Embry-Riddle UAV Initiative
  • Multi-year plan
  • Implement enabling technology
  • Distributed Flight Control System (DFCS)
  • Focal point for research projects
  • CE, EE, CS, AE
  • Primary target low cost
  • Industrial/educational applications
  • UAV Helicopter - 20k

4
Background
  • Started Unmanned Aerial Vehicle
  • NASA coined Unattended
  • Meaning no pilot or remote control
  • Major problem with UAVs today
  • Built around one centralized computer
  • Complex design
  • Error prone
  • Not easily adaptable
  • Lacks robustness

5
Full Scope of Research
  • Main Objective
  • Define a suitable Inertial Navigation System for
    our UAV
  • Primary criteria
  • High short-term performance
  • /- 1 or better over 10 s
  • /- 10 ft in pos. over 10s
  • Inexpensive
  • Lightweight
  • Limited useable load
  • Low power consumption
  • Limited onboard power

6
Tracking UAV Movement
  • Instrument Inertial Measuring Unit (IMU)
  • Sensor cluster and sampling circuits
  • Navigation computer
  • Performs filtering and navigation calculations
  • Strapdown Inertial Navigation System
  • Rigidly fixed to body no gimbals
  • Combines IMU and navigation computer
  • Attitude Heading Reference System (AHRS)

7
Inertial Measuring Unit
  • Orthogonal sensor cluster
  • Rate gyros and accelerometers
  • MEMS sensors satisfy criteria

8
Navigation Computer
  • Data filtering
  • Kalman filter
  • Statistical method
  • Reduces noise and sensor errors
  • Coordinate Transformation
  • Directional Cosine Matrices (DCM)
  • Body to Navigation

9
The AHRS
  • Accelerometers
  • Range
  • /- 0.5 gs
  • Resolution
  • 12-bit - 0.2 mg
  • Gyroscopes
  • Range
  • /- 25 /s
  • Resolution
  • 12-bit - .01 /s
  • Full updates at no less than 10 Hz
  • Heading, Roll, Pitch, and Yaw, velocity, and
    position

10
Future work
  • Senior project
  • Build and test AHRS
  • Couple AHRS with DGPS
  • Bound the sensor errors
  • Full UAV navigation solution

11
Special Thanks
  • Dr. Gary Gear Faculty Mentor
  • Dr. David Viger and David Brandstein
  • - McNair Director and Coordinator
  • College of Engineering Faculty
  • Embry-Riddle Aeronautical University

McNair Scholars Program
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