2015
DOI: 10.1115/1.4029464
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Position–Yaw Tracking of Quadrotors

Abstract: A yaw angle, different from zero, introduces highly nonlinear couplings in the rotational and translational quadrotor dynamics, implying undesirable motions. This argument has motivated that the position control problem of quadrotors is studied generally regulating yaw at zero. However, zeroing yaw limits the maneuverability of underactuated quadrotors because yaw is one of the four actuated motions. In this paper, the simultaneous tracking of position and time-varying heading is proposed, based on an integral… Show more

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Cited by 29 publications
(24 citation statements)
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“…This can be done by commanding the desired yaw of each multirotor with the inverse kinematics of the flying structure. The yaw control is expected to be realized with recent works about yaw-tracking [1], [83], feasible environment interaction must be researched, and a good starting point is [87], also the aforementioned papers.…”
Section: Concluding Remarks and Future Workmentioning
confidence: 99%
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“…This can be done by commanding the desired yaw of each multirotor with the inverse kinematics of the flying structure. The yaw control is expected to be realized with recent works about yaw-tracking [1], [83], feasible environment interaction must be researched, and a good starting point is [87], also the aforementioned papers.…”
Section: Concluding Remarks and Future Workmentioning
confidence: 99%
“…• To develop a suitable mathematical model and the adequate controller; this could be based on [1], [83], [69], [65] investigations. • To develop a way for transmitting force among underactuated flying machines [87].…”
Section: Research Is Needed Inmentioning
confidence: 99%
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