2019 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS) 2019
DOI: 10.1109/iros40897.2019.8967725
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Design, Modeling and Control of Fully Actuated 2D Transformable Aerial Robot with 1 DoF Thrust Vectorable Link Module

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Cited by 26 publications
(15 citation statements)
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“…It can grasp objects of different shapes properly adapting its configuration [104]. An evolution of such a vehicle used for manipulation tasks has been presented in [117] and [106].…”
Section: ) Multirotor Morphing (M)mentioning
confidence: 99%
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“…It can grasp objects of different shapes properly adapting its configuration [104]. An evolution of such a vehicle used for manipulation tasks has been presented in [117] and [106].…”
Section: ) Multirotor Morphing (M)mentioning
confidence: 99%
“…Again the platform configuration is optimized to minimize the masscenter offset between the platform and the payload reducing steady-state hovering torque. An evolution of such a vehicle that is fully-actuated has been presented in [117].…”
Section: Interconnected Actuated Multibody Designsmentioning
confidence: 99%
“…It is necessary to check the comprehensive motion in all three axes. Therefore an extended quantity called feasible control torque convex q ( ) T (Anzai et al, 2019;Park et al, 2018) is applied to validate the rotational controllability which is given by τ τ…”
Section: Valid Transformation Rangementioning
confidence: 99%
“…We found that a net force with variable direction in a three-dimensional force space is the key to overcoming the singularity. Then, [8] proposed a vectoring apparatus for propellers that can generate a lateral component force with variable direction; they also developed a prototype composed of six links embedded with this propeller apparatus to achieve flight stability in a fully-actuated manner. However, the singularity issue is not addressed in this previous work.…”
Section: Introductionmentioning
confidence: 99%
“…However, a crucial shortcoming of such an apparatus is that it cannot generate lateral force in arbitrary directions. In contrast, the apparatus proposed by [8], named a yawvectoring apparatus, has a vectoring axis perpendicular to the plane of the two-dimensional multilinked model and also has a rotor mount tilted from the vectoring axis at a fixed angle to yield the lateral component force. It is notable that, the vectoring angles cannot be easily used as a control input, because the opposite lateral component force demands the apparatus to rotate 180 • back and forth at a high rate, thereby making the flight significantly unstable.…”
Section: Introductionmentioning
confidence: 99%