2018 4th Iranian Conference on Signal Processing and Intelligent Systems (ICSPIS) 2018
DOI: 10.1109/icspis.2018.8700556
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Autonomous Flight of Quadcopters in the Presence of Ground Effect

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Cited by 4 publications
(5 citation statements)
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“…Coordinate frames transformation is used to transform quantities between the two reference frames. To avoid the nonlinearity, geometric singularity, and computational cost usually associated with the Euler angles [28], [29], the quaternion approach is applied for coordinate frames transformation. A quaternion is a hyper-complex number with four dimensions that include a scalar part q o , and a threedimensional vector part ⃗ q = [q i , q j , q k ] with orthonormal base [i, j, k] [30].…”
Section: Quaternion-based Mathematical Model Of Quadrotor Uav a Preli...mentioning
confidence: 99%
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“…Coordinate frames transformation is used to transform quantities between the two reference frames. To avoid the nonlinearity, geometric singularity, and computational cost usually associated with the Euler angles [28], [29], the quaternion approach is applied for coordinate frames transformation. A quaternion is a hyper-complex number with four dimensions that include a scalar part q o , and a threedimensional vector part ⃗ q = [q i , q j , q k ] with orthonormal base [i, j, k] [30].…”
Section: Quaternion-based Mathematical Model Of Quadrotor Uav a Preli...mentioning
confidence: 99%
“…6R is considered as Out of Ground Effect (OGE) where GE is typically doesn't exist. Experiments show that at constant power, GE is mathematically expressed as [37], [44]…”
Section: B Quadrotor Flight Dynamics Modelingmentioning
confidence: 99%
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“…First of all, an explanation of the thrust in the phases of take-off and landing, and then in the phase of hovering, is given. [17] Thrust is a force perpendicular to the plane of the propeller. It is created by rotating the rotor at a certain speed.…”
Section: Thrust In Different Phases Of Flightmentioning
confidence: 99%
“…In simpler terms, the dynamics of the response depends on the number of revolutions of the engine. [17] From everything presented, the researchers came to the conclusion that there is no dependence on the time constant of the number of revolutions of the engine thrust in relation to the height from the ground when there is only one active rotor.…”
Section: Dynamic Analysis Of the Ground Effect At Low Speedsmentioning
confidence: 99%