2014 IEEE International Symposium on Safety, Security, and Rescue Robotics (2014) 2014
DOI: 10.1109/ssrr.2014.7017669
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A nonparallel hexrotor UAV with faster response to disturbances for precision position keeping

Abstract: This paper presents a fully actuated UAV platform with a nonparallel design. Standard multirotor UAVs equipped with a number of parallel thrusters would result in underactuation. Fighting horizontal wind would require the robot to tilt its whole body toward the direction of the wind. We propose a hexrotor UAV with nonparallel thrusters which results in faster response to disturbances for precision position keeping. A case study is presented to show that hexrotor with a nonparallel design takes less time to res… Show more

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Cited by 41 publications
(13 citation statements)
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“…This SmQ system, yet, still cannot exert a downward force larger than its own weight due to the unilateral thrust generation of the standard drones. More closely related to our proposed ODAR system are the designs of [10]- [14], where rotors attached with nonparallel directions are used to attain the full-actuation on SE (3) with no extra actuation. The works of [10]- [12] however optimize (or adjust) only the direction of the six rotors in S 1 while leaving their positions to be the same as those of the standard hexarotors.…”
mentioning
confidence: 99%
“…This SmQ system, yet, still cannot exert a downward force larger than its own weight due to the unilateral thrust generation of the standard drones. More closely related to our proposed ODAR system are the designs of [10]- [14], where rotors attached with nonparallel directions are used to attain the full-actuation on SE (3) with no extra actuation. The works of [10]- [12] however optimize (or adjust) only the direction of the six rotors in S 1 while leaving their positions to be the same as those of the standard hexarotors.…”
mentioning
confidence: 99%
“…In particular, by using matrix multiplication as the group operation, the attitude error R e = RR T p , is employed as the attitude error measure in SO (3), which was already introduced in equation (22). The error kinematics can be derived from (4) and (13) as follows:…”
Section: B Control Torque and Attitude Error Dynamicsmentioning
confidence: 99%
“…By designing an actuation mechanism that can change the thrust direction, a net force can be produced with respect to the aircraft frame, which allows to handle more complex maneuvering. Thrust-vectoring UAVs can be realized by mounting the propellers in a non-coplanar fashion [4], [13], [24], [25] or by employing servo-actuators to dynamically adjust their orientation [8], [9], [23], [27]. While the dynamically tiltable configuration is efficient in terms of power consumption and may achieve full actuation [27], it has a more complex mechanical structure.…”
Section: Introductionmentioning
confidence: 99%
“…Therefore, passively tilted non-flat configuration is more suitable for analysis and realization. Furthermore, an analysis of the tilt angle parameter is given in [10]. The drawback of the presented papers is a limitation in the mathematical representation of the multirotor configuration, so the analysis is also restricted to specific multirotor parameters.…”
Section: Introductionmentioning
confidence: 99%