2007
DOI: 10.1109/robot.2007.363072
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Stabilization of a Small Unmanned Aerial Vehicle Model without Velocity Measurement

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Cited by 13 publications
(5 citation statements)
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“…The interest in UAVs systems woke because a pilot aboard the aircraft is not required, allowing the use of smaller aircraft, with lower power requirements. These systems can perform dangerous missions in hostile environments or under adverse weather conditions without compromising the physical integrity of the pilot [3]. Nowadays, Searching and Rescue CENTUM company dedicated to developing engineering projects and specialty technology products, developed an unmanned vehicle with a search system in emergency situations.…”
Section: Vertical Takeoff and Landing Vehiclesmentioning
confidence: 99%
“…The interest in UAVs systems woke because a pilot aboard the aircraft is not required, allowing the use of smaller aircraft, with lower power requirements. These systems can perform dangerous missions in hostile environments or under adverse weather conditions without compromising the physical integrity of the pilot [3]. Nowadays, Searching and Rescue CENTUM company dedicated to developing engineering projects and specialty technology products, developed an unmanned vehicle with a search system in emergency situations.…”
Section: Vertical Takeoff and Landing Vehiclesmentioning
confidence: 99%
“…Un tetramotor es un sistema multivariable que cuenta con seis grados de libertad (x, y, z,pitch, roll y yaw) y subactuado ya que consta de menos actuadores que grados de libertad. Los rotores del tetramotor producen las fuerzas y momentos principales que actúan sobre este, Figura 3 [1]. El balance del torque total del sistema se logra debido a que dos pares de motores rotan en direcciones opuestas.…”
Section: Principio De Operación Del Tetramotorunclassified
“…Consequently, the dynamic model has the translational velocity vector given by and the rotational velocity vector represented by . The Kinematic model of the quadrotor is [24]: (1) Where and are the transformation velocity matrices between I i and I B respectively. Using the first and the second Newton's laws on the flight system when it is subject to forces and moments, applied to the center of gravity (COG) of the body, one can get the two sub-dynamic model as follows:…”
Section: Dynamic Model Of the Uavmentioning
confidence: 99%
“…For this reasons, numerous nonlinear control design methods (feedback linearization, backstepping, sliding mode, etc.) have been proposed in recent studies [1][2][3][4][5][6][7][8].…”
Section: Introductionmentioning
confidence: 99%