![]() ![]() In this paper, we develop a flight dynamics model of this drone. The flight stability and control of the entire drone is achieved using the net thrust produced by the quadcopters rotors and is controlled using a central flight controller which determines the required titling angles and rotational speeds of each quadcopter. The tilting of each of the quadcopters is achieved using the rotors of the quadcopter itself and controlled using its flight controller. It is believed to encompass several advantages, including enhanced stability, horizontal flight, and a wide stabilized platform which can be used for in- flight power generation and payload. This new design concept of a drone is not limited to a swarm of four quadcopters and can be extended to two or more. This conceptual drone is one that is composed of four quadcopters connected to a rigid frame and allowed to tilt about a revolute hinge attached to the frame. School of Engineering Emirates Aviation University Dubai, UAE.Ībstract This paper presents the modelling and simulation of the flight dynamics of four physically linked, tilting quadcopters. Jaidev Sanketi, Rishika Kasliwal, Srinivasa Raghavan, Sundus Awan ![]() Modelling and Simulation of a Multi-Quadcopter Concept
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