Flyability Sa

Ecole Polytechnique Federale De Lausanne

Ecole Polytechnique Féderale De Lausanne (epfl)

Ludovic Daler

Adrien Briod

Arnaud Garnier

Alexandre Pabouctsidis

Dario Floreano

Stefano Mintchev

Pierre-Etienne Bourban

Antonino Sidoti

Mathieu Valceschini

Joel Cugnioni

Orsika Bojtar

Stefano Zampieri

Veronique Michaud

Véronique Michaud

An unmanned aerial vehicle for non-destructive testing includes: an outer protective cage, a propulsion system mounted inside the outer protective cage and fixed thereto, an arm having a first end attached to the outer protective cage, and a non-destructive testing sensor mounted at a second end of the arm. The arm extends outward from the outer protective cage, the arm having a length between 1 and 50 percent of an overall linear dimension of the outer protective cage.

Unmanned aerial vehicle

Vertical take off and landing unmanned aerial vehicle (UAV) comprising a multi-propeller propulsion system ('the system'), an outer protective cage surrounding the system, an autonomous power source, a sensing system, and a control system. The sensing system has an orientation sensor and a displacement sensor. The system has at least two propellers spaced apart in a non-coaxial manner. The control system controls the flight or hovering of the UAV. The control system reverses thrust on at least one propeller distal from a point of contact with an obstacle while controlling a motor of a proximal propeller from the contact point to generate lift, the thrust of the distal and proximal propellers being controlled to exert lift on the UAV to counteract gravitational force thereon and apply a moment of rotation about the point of contact to stabilize the position of the UAV or to counteract torque resulting from inertia.

Unmanned aerial vehicle with collision tolerant propulsion and controller

Unmanned aerial vehicle (UAV) including an inner frame, an inner flight propulsion system mounted on the inner frame, an outer frame, a gimbal system comprising at least two rotational couplings coupling the inner propulsion system to the outer frame, a control system, a power source, and an outer frame actuation system configured to actively orient the outer frame with respect to the inner frame.

Unmanned aerial vehicle with protective outer cage

Unmanned aerial vehicle (UAV) including a flight propulsion system and a support system coupled to the flight propulsion system, the support system comprising a protective outer cage configured to surround the flight propulsion system, wherein the outer cage comprises a plurality of cage frame modules that are manufactured as separate components and assembled together to form at least a portion of the outer cage configured to surround the flight propulsion system.

Unmanned aerial vehicle and protective outer cage therefor

A VTOL (vertical take-off and landing) aerial flying vehicle comprising an inner frame, a gimbal system and an outer frame, the inner frame comprising a propulsion system and a control system. The propulsion system being able to generate a lift force. The VTOL may also include a decoupling mechanism having either a linear or non-linear beam coupled to a ring. The beam may optionally include sliders at ends thereof that provide an additional rotation freedom to the inner frame.

Vertical take-off and landing aerial vehicle

An aerial vehicle including self-autonomous deployable arms and methods of deploying the vehicle are disclosed. The arms may include patterns located thereon that allow the arms to transition between wrapped, flat, and deployed configurations autonomously without the need for direct intervention by a user.

Growing community of inventors

Lausanne, Switzerland

Ludovic Daler