Files in this item

FilesDescriptionFormat

application/pdf

application/pdftechnical_report.pdf (175kB)
(no description provided)PDF

Description

Title:Kinematic Model for Fixed-Wing Aircraft with Constrained Roll-Rate
Author(s):Theile, Mirco; Yu, Simon
Subject(s):Kinematic Model
Fixed-Wing Aircraft
Trajectory Estimation
Constrained Roll Rate
UAV
Abstract:The technical report derives a kinematic model of fixed-wing aircraft that is based on constrained roll rate. This new kinematic model can be used for trajectory planning and optimization.
Issue Date:2018-09-15
Genre:Technical Report
Type:Text
Language:English
URI:http://hdl.handle.net/2142/101442
Sponsor:National Science Foundation (NSF), CNS-1646383
Date Available in IDEALS:2018-09-21


This item appears in the following Collection(s)

Item Statistics