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Determining of correlation relationship between roll, pitch, and yaw for UAVs Cover

Determining of correlation relationship between roll, pitch, and yaw for UAVs

Open Access
|May 2019

Figures & Tables

Figure 1

UAV ‘Arrow’ aircraft type

Table 1

The technical characteristics of the UAV ‘Arrow’

CharacteristicsParameters
Digital cameraSony QX1
Take-off weight [kg]4.8
Battery capacity [Ah]16
Minimum flight speed [km/h]50
Cruising flight speed [km/h]60–80
Maximum flight time [min]100
Maximum flight range [km]100
Maximum controlled distance from the base [km]15
Maximum flight altitude [m]5000
Minimum operational altitude [m]75
The maximum image resolution [sm/px]2
Dimensions in transportation configuration [sm]120 × 25 × 25
Limiting wind speed [m/s]12
Figure 2

Correlation diagram ĸ and α

Figure 3

Correlation diagram α and ω

Figure 4

Correlation diagram ĸ and ω

Figure 5

Empirical regression lines

Table 2

Coefficient of multiple correlation

Regression statistics
R0.378
R20.143
Standardized R20.125
Table 3

Parameters of the regression model

Coeff. of regr. modelStandard Errort-statisticP-valueLower 95%Upper 95%
a04.4821.7590892.54780.01244440.98967.9741
a1-1.2330.312375-3.94690.0001517-1.8530-0.6128
a2-0.2480.228563-1.08510.2806222-0.70180.2057
Table 4

Dispersion analysis

dfSSMSF-valueSignificance level F
Factors (m)21046.16831523.08415517.9372867510.000649162
Residue956260.7029765.90213653
nm – 1977306.871281
DOI: https://doi.org/10.2478/rgg-2019-0002 | Journal eISSN: 2391-8152 (formerly 0867-3179) | Journal ISSN: 0867-3179
Language: English
Page range: 13 - 18
Submitted on: Sep 7, 2018
Accepted on: Mar 15, 2019
Published on: May 11, 2019
Published by: Warsaw University of Technology
In partnership with: Paradigm Publishing Services
Publication frequency: 2 issues per year

© 2019 Volodymyr Hlotov, Alla Hunina, Mariana Yurkiv, Zbigniew Siejka, published by Warsaw University of Technology
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.