Mathematical Problems in Engineering / 2013 / Article / Tab 1

Research Article

Supervising Control for Unmanned Aerial Vehicles

Table 1

Data of UAV.

SymbolValueDescription

0.147Coefficient of lift with zero angle of attack
4.54Lift due to change in angle of attack
1.972Lift due to change in rate of angle of attack
0.37Lift due to change in elevator deflection
5.54Lift due to change in pitching moment
0.0434Zero drag
0.001Coefficient of damping due to forward speed
0.0Drag due to change in elevator deflection
−0.83Side force due to change in side slip angle
0.0Side force due to change in aileron deflection
0.1914Side force due to change in rudder deflection
0.0085Side force due to roll rate
0.25Side force due to yaw rate
0.0001Pitching moment with zero angle of attack
−0.39Pitching moment due to change in alpha
0.0002Pitching moment due to forward speed
−4.37Pitching moment due to rate of alpha
1.2289Pitching moment due to elevator deflection
−38.201Pitching moment due to q
−0.022Roll moment due to side slip angle
0.34Roll moment due to aileron deflection
0.0154Roll moment due to rudder deflection
−0.3819Roll moment due to p
0.0514Roll moment due to r
0.1022Yaw moment due to side slip angle
−0.0088Yaw moment due to aileron deflection
−0.1404Yaw moment due to rudder deflection
−0.017Yaw moment due to p
−0.28Yaw moment due to r
30Mass of UAV (lbs)
10.9Wing surface area (sq ft)
7.92Wing span (ft)
1.5Mean chord length (ft)
1.08Moment of inertia about X axis (slug-ft2)
2.01Moment of inertia about Y axis (slug-ft2)
3.03Moment of inertia about Z axis (slug-ft2)
0.0Product of inertia XY axis (slug-ft2)
0.0Product of inertial YZ axis (slug-ft2)
0.0Product of inertia XZ axis (slug-ft2)

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