7 accepted papers
In this work, a collaborative co-evolution approach is adopted to solve a joint physical design and feedback control optimization problem of a nature-inspired Unmanned Aerial Vehicle (UAV). Unlike traditional multirotors and fixed-wing aircraft, lift is achieved by spinning its entire body with atta
In this paper, the high angular rate estimation for simultaneous localisation and mapping (SLAM) of a Flying Li-DAR (Flydar) is presented. The proposed EKF-based algorithm exploits the sinusoidal magnetometer measurement generated by the continuously rotating airframe for estimation of the robot hov…
In this letter, the design optimization and localization with sparse sensing array of range-based sensors are presented. This optimization focuses on an optimized sparse sensing array for localization and autonomous navigation in tunnel environments with right rectangular prism geometry and the auto
To deliver lightweight sensor payloads to disaster-struck areas by means of an aerial deployment, a novel bio-inspired method capitalizing on autorotation to slow down vertical descent rate is proposed. This concept is illustrated using the samara autorotating wing (SAW) platform, which features a u
The seeds of Maple trees (Samara) use autorotation as a unique mechanism to disperse their seeds. By exploiting gyroscopic stability of a spinning wing, the Samara is able to cover large horizontal distance despite having no form of propulsion. We applied and adapted this natural ability in our nove…
The seeds of Maple trees (Samara) use autorotation as a unique mechanism to disperse their seeds. By exploiting gyroscopic stability of a spinning wing, the Samara is able to cover large horizontal distance despite having no form of propulsion. We applied and adapted this natural ability in our nove
This paper describes the Transformable HOvering Rotorcraft (THOR), a prototype Unmanned Aerial Vehicle (UAV) that explores a novel approach in combining the range and speed of a horizontal flying platform with the hovering and maneuverability of a rotor-wing. This is achieved by integrating a taille…