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Proceedings ArticleDOI

Quadrotor hoverboard

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TLDR
A control scheme that uses the center of gravity (CoG) variation caused by the tilt of the pilot standing on a quadrotor to maneuver it in the horizontal plane is proposed and simulation results show that it is possible to control the Quadrotor motion using CoG shifts caused by a pilot with moderate skills.
Abstract
Riding on a quadrotor in a standing position demands extreme piloting skills. However, niche tasks like certain inspection and rescue missions can be accomplished by doing so. In this paper, we propose a control scheme that uses the center of gravity (CoG) variation caused by the tilt of the pilot standing on a quadrotor to maneuver it in the horizontal plane. Keeping potential applications in mind, we design controllers for two modes of operation: a) Maneuver via leaning mode during which the quadrotor converts the forward CoG shift into a proportional forward speed, and the sideward CoG shift to a yaw rate, thus enabling a turn, and b) Remote control mode in which the quadrotor platform rejects all the disturbances including the pilot’s movements and maintains the desired speed and turn commands provided by the pilot using a hand-held remote control. We use a simplified model of a human standing on a quadrotor to test the proposed control laws using simulations. The simulation results show that it is possible to control the quadrotor motion using CoG shifts caused by a pilot with moderate skills.

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Citations
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Proceedings ArticleDOI

A Flying Inverted Pendulum With Unknown Length

TL;DR: In this paper , a concurrent learning adaptive controller is used to balance the inverted pendulum on a quadrotor with unknown length of the pendulum, where the control input cannot be used to cancel the uncertainty.
Proceedings ArticleDOI

A Flying Inverted Pendulum With Unknown Length

TL;DR: In this article , a concurrent learning adaptive controller is used to balance the inverted pendulum on a quadrotor with unknown length of the pendulum, where the control input cannot be used to cancel the uncertainty.
References
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Proceedings ArticleDOI

A flying inverted pendulum

TL;DR: This work extends the classic control problem of the inverted pendulum by placing the pendulum on top of a quadrotor aerial vehicle, using a ‘Virtual Body Frame’ for the time-invariant description of curved trajectories.
Journal ArticleDOI

Mathematical Modelling and Control of an Unmanned Aerial Vehicle with Moving Mass Control Concept

TL;DR: This paper presents a complete nonlinear dynamical model of a multi-rotor unmanned aerial vehicle and uses it to derive the transfer functions of roll and pitch dynamics and derives necessary conditions for testbed parameters in order to match the testbed and free-flight quadrotor dynamics.
Journal ArticleDOI

Cascaded control for balancing an inverted pendulum on a flying quadrotor

TL;DR: A three loop cascade control strategy is proposed based on active disturbance rejection control (ADRC) and both the pendulum balancing and the trajectory tracking of the flying quadrotor are implemented by using the proposed control strategy.
Proceedings ArticleDOI

Design considerations for a large quadrotor with moving mass control

TL;DR: In this paper, the authors proposed using miniature two stroke internal combustion engines to supply the necessary lift and endurance and combine them with a novel control concept based on the variations of the center of gravity (CoG) of the system.
Book ChapterDOI

Recent and Future Developments

TL;DR: The state-of-the-art technology in energy harvesting is the wind powered and photovoltaic technologies in the century as discussed by the authors, and activities like the solar harness UAVs are ongoing.