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Spline Trajectory Algorithm Development: Bezier Curve Control Point Generation for UAVsA greater need for sophisticated autonomous piloting systems has risen in direct correlation with the ubiquity of Unmanned Aerial Vehicle (UAV) technology. Whether surveying unknown or unexplored areas of the world, collecting scientific data from regions in which humans are typically incapable of entering, locating lost or wanted persons, or delivering emergency supplies, an unmanned vehicle moving in close proximity to people and other vehicles, should fly smoothly and predictably. The mathematical application of spline interpolation can play an important role in autopilots' on-board trajectory planning. Spline interpolation allows for the connection of Three-Dimensional Euclidean Space coordinates through a continuous set of smooth curves. This paper explores the motivation, application, and methodology used to compute the spline control points, which shape the curves in such a way that the autopilot trajectory is able to meet vehicle-dynamics limitations. The spline algorithms developed used to generate these curves supply autopilots with the information necessary to compute vehicle paths through a set of coordinate waypoints.
Document ID
20160010151
Acquisition Source
Langley Research Center
Document Type
Conference Paper
External Source(s)
Authors
Howell, Lauren R.
(Alabama Univ. Tuscaloosa, AL, United States)
Allen, B. Danette
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 9, 2016
Publication Date
June 13, 2016
Subject Category
Aircraft Design, Testing And Performance
Aircraft Communications And Navigation
Numerical Analysis
Report/Patent Number
NF1676L-22921
AIAA Paper 2016-4197
Meeting Information
Meeting: AIAA Aviation Technology, Integration, and Operations Conference (2016 AIAA Aviation)
Location: Washington, DC
Country: United States
Start Date: June 13, 2016
End Date: June 17, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 432938.09.01.07.98.02
Distribution Limits
Public
Copyright
Public Use Permitted.
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