Development of control system algorithms for mini unmanned aerial vehicle of combined scheme — convertiplane

We propose the description of algorithms and computational techniques accelerating the calculation of orientation, stabilization, approximate estimate of the wind velocity with the use of the software as applied to the designed mini unmanned aerial vehicle of the combined scheme, namely, the convert...

Full description

Saved in:
Bibliographic Details
Published in:Russian aeronautics 2012-04, Vol.55 (2), p.199-202
Main Authors: Syzdykov, E. K., Gainutdinova, A. V., Krikun, K. G.
Format: Article
Language:English
Subjects:
Algorithms
Approximation
Automotive Engineering
Computer programs
Engineering
Mathematical analysis
Mini
Stabilization
Technical Notes Flight Vehicle Design
Unmanned aerial vehicles
Wind velocity
Citations: Items that cite this one
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
Description
Summary:We propose the description of algorithms and computational techniques accelerating the calculation of orientation, stabilization, approximate estimate of the wind velocity with the use of the software as applied to the designed mini unmanned aerial vehicle of the combined scheme, namely, the convertiplane, that is capable to takeoff and land vertically, hover, and fly as an airplane.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799812020146