University of Illinois Urbana-Champaign

Kinematic Model for Fixed-Wing Aircraft with Constrained Roll-Rate

Theile, Mirco; Yu, Simon

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https://hdl.handle.net/2142/101442

Description

Title
Kinematic Model for Fixed-Wing Aircraft with Constrained Roll-Rate
Author(s)
  • Theile, Mirco
  • Yu, Simon
Issue Date
2018-09-15
Keyword(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.
Type of Resource
text
Language
en
Permalink
http://hdl.handle.net/2142/101442
Sponsor(s)/Grant Number(s)
National Science Foundation (NSF), CNS-1646383

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Research and Tech Reports - Computer Science