51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2013
DOI: 10.2514/6.2013-1092
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Modeling and Attitude Control Analysis of a Spherical VTOL Aerial Vehicle

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Cited by 8 publications
(4 citation statements)
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“…When the power is low, it can use the rolling mode to roll omnidirectionally on the ground. Following JFS, the typical structures of single propeller and control blade are BYFQ 57 (as shown in Figure 14(b)), UFRO 58 (as shown in Figure 14(c)), TVAC 59 (as shown in Figure 14(d)), and UNI-copter 60 (as shown in Figure 14(e)). Beyer and Costello 61 proposed a micro coaxial two propeller robot hopping Rotochute (as shown in Figure 14(f)) with flying and jumping capabilities for complex environments such as caves and collapsed buildings.…”
Section: Classification and Research Status Of Spherical Mobile Robot...mentioning
confidence: 99%
“…When the power is low, it can use the rolling mode to roll omnidirectionally on the ground. Following JFS, the typical structures of single propeller and control blade are BYFQ 57 (as shown in Figure 14(b)), UFRO 58 (as shown in Figure 14(c)), TVAC 59 (as shown in Figure 14(d)), and UNI-copter 60 (as shown in Figure 14(e)). Beyer and Costello 61 proposed a micro coaxial two propeller robot hopping Rotochute (as shown in Figure 14(f)) with flying and jumping capabilities for complex environments such as caves and collapsed buildings.…”
Section: Classification and Research Status Of Spherical Mobile Robot...mentioning
confidence: 99%
“…Figure 6. View of encased drones, (a) Spherical Drone [166], (b, c) UFRO [167], (d) Glimball [168], (e, f) PRSS UAV [169], (g) Simha et al's Drone [170], (h) Spherical Drone [171], and (i, j) isphere [172].…”
Section: Suitable Drone Configuration For Underground Mining Applicatmentioning
confidence: 99%
“…An attitude controller of the SUAV is able to attain a desired position on the X and Y axes, since the movements along the X and Y axes are accompanied by controlling θ and ϕ. The combination of the frame area of the SUAV and the reaction torque produced by the motor speed is used for ψ control [5]. The key in this work is the control of θ and ϕ using the torque generated by varying the CG.…”
Section: A Center-of-gravity Variationmentioning
confidence: 99%
“…Malandrakis et al and Loh and Jacob demonstrated SUAVs consist of a contrarotating (parts of a mechanism rotate in opposite directions about a common axis) motor and several control vanes [5,6]. The contrarotating motor is used to minimize the reaction torque generated by the motor rotation, and a classical proportional-integral-derivative (PID) control law is applied for attitude control.…”
Section: Introductionmentioning
confidence: 99%