Aircraft landing using dynamic 2D image-based guidance control

UM > Faculty of Science and Technology > DEPARTMENT OF ELECTRICAL AND COMPUTER ENGINEERING

Status	已發表Published
	Aircraft landing using dynamic 2D image-based guidance control
	Tang, Z; Cunha, R; Hamel, T; Silvestre, C
	2019-10-01
Source Publication	IEEE Transactions On Aerospace and Electronic Systems
ISSN	0018-9251
Pages	2104 -2117
Abstract	This work proposes a 2D image-based controller to automatically steer a fixed-wing Unmanned Aerial Vehicle (UAV) during the first three stages of landing: alignment, glide-slope, and flare. Observable image features of the runway and its textured ground are exploited to derive a feedback controller for the automatic maneuver. The proposed controller ensures the horizontal position alignment and a smooth touchdown of the aircraft without estimating the height above the runway. In addition, the 2D image-based control structure adopted also enforces wind disturbance rejection, without the need for an explicit wind estimator. Simulation results are presented to illustrate the performance of the controller.
Keyword	2D image-based feedback control optical flow automatic landing fixed-wing unmanned aerial vehicle.
Language	英語English
The Source to Article	PB_Publication
PUB ID	42400
Document Type	Journal article
Collection	DEPARTMENT OF ELECTRICAL AND COMPUTER ENGINEERING
Recommended Citation GB/T 7714	Tang, Z,Cunha, R,Hamel, T,et al. Aircraft landing using dynamic 2D image-based guidance control[J]. IEEE Transactions On Aerospace and Electronic Systems, 2019, 2104 -2117.
APA	Tang, Z., Cunha, R., Hamel, T., & Silvestre, C (2019). Aircraft landing using dynamic 2D image-based guidance control. IEEE Transactions On Aerospace and Electronic Systems, 2104 -2117.
MLA	Tang, Z,et al."Aircraft landing using dynamic 2D image-based guidance control".IEEE Transactions On Aerospace and Electronic Systems (2019):2104 -2117.

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