UAV Automatic Landing Control Law

Abstract:

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Landing is the most important stage of the Flight of UAV, the study of automatic landing of UAVs has important engineering significance. In this paper, the UAV landing trajectory is divided into approach phase, steep glide phase and flare phase; a cascade control structure controller of height tracking was applied and the landing control law was designed. The digital simulation was done in the MATLAB / simulink environment. The results of simulation indicated that UAV can track the designed landing trajectory very well under the control law of automatic landing and safe landing can be achieved.

Info:

Periodical:

Advanced Materials Research (Volumes 383-390)

Edited by:

Wu Fan

Pages:

1452-1457

DOI:

10.4028/www.scientific.net/AMR.383-390.1452

Citation:

M. H. Liu et al., "UAV Automatic Landing Control Law", Advanced Materials Research, Vols. 383-390, pp. 1452-1457, 2012

Online since:

November 2011

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Price:

$35.00

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