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Dynamics and Control of Quadcopter in Uncertain EnvironmentWe consider problem of dynamics, control, and uncertainty quantification for quadcopter. We use the 6DOF model of quadcopter dynamics, linear quadratic regulator and linear quadratic Gaussian control of quadcopter in the presence of dynamical disturbances, measurement noise, hidden dynamical variables, dashing GPS signal, and wind gusts to predict quadcopter trajectory. We identify key sources of uncertainties and report on progress in development of a system that estimates the probability of safety-critical events using a set of algorithms based on the trajectory predictions.
Document ID
20180006836
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Luchinsky, D. G.
(SGT, Inc. Moffett Field, CA, United States)
Schuet, S. R.
(NASA Ames Research Center Moffett Field, CA, United States)
Goebel, K.
(GE Global Research Center Niskayuna, NY, United States)
Date Acquired
October 25, 2018
Publication Date
September 24, 2018
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN54034
Meeting Information
Meeting: Annual Conference of the Prognostics and Health Management Society 2018
Location: Philadelphia, PA
Country: United States
Start Date: September 24, 2018
End Date: September 27, 2018
Sponsors: Prognostics and Health Management Society (PHM)
Funding Number(s)
CONTRACT_GRANT: NNA14AA60C
CONTRACT_GRANT: IPA08-NA
WBS: WBS 00370.03C.112.001
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
uncertainty quantification
LQG
LQR
quadrotor
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