contributor author | Kamesh | |
contributor author | Subbarao | |
contributor author | Mousumi | |
contributor author | Ahmed | |
date accessioned | 2017-05-08T21:34:09Z | |
date available | 2017-05-08T21:34:09Z | |
date copyright | May 2014 | |
date issued | 2014 | |
identifier other | %28asce%29as%2E1943-5525%2E0000275.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/56426 | |
description abstract | In this paper, a backstepping-based nonlinear guidance controller is developed, designed for three-dimensional trajectory tracking for an unmanned aerial vehicle. The guidance law design assumes first-order dynamics for the speed, course/heading, and flight path angles. The three-dimensional kinematic model is simplified to yield a seemingly decoupled system that separates the course/heading from the flight path angle. A closed loop stability of the guidance laws via Lyapunov analysis is demonstrated, and the efficacy of the controller is illustrated for three representative cases. | |
publisher | American Society of Civil Engineers | |
title | Nonlinear Guidance and Control Laws for Three-Dimensional Target Tracking Applied to Unmanned Aerial Vehicles | |
type | Journal Paper | |
journal volume | 27 | |
journal issue | 3 | |
journal title | Journal of Aerospace Engineering | |
identifier doi | 10.1061/(ASCE)AS.1943-5525.0000275 | |
tree | Journal of Aerospace Engineering:;2014:;Volume ( 027 ):;issue: 003 | |
contenttype | Fulltext | |