Static Hovering Realization for Multirotor Aerial Vehicles With Tiltable Propellers

Author:

Hamandi Mahmoud1,Seneviratne Lakmal2,Zweiri Yahya3

Affiliation:

1. Khalifa University Department of Aerospace Engineering, Khalifa University Center for Autonomous, Robotic Systems (KUCARS), , Abu Dhabi , United Arab Emirates

2. Khalifa University Department of Mechanical Engineering, and Director of Khalifa University Center for Autonomous Robotic Systems (KUCARS), , Abu Dhabi , United Arab Emirates

3. Khalifa University Department of Aerospace Engineering, Advanced Research and Innovation Center (ARIC), , Abu Dhabi , United Arab Emirates

Abstract

Abstract This paper presents a theoretical study on the ability of multirotor aerial vehicles (MRAVs) with tiltable propellers to achieve and sustain static hovering at different orientations. To analyze the ability of MRAVs with tiltable propellers to achieve static hovering, a novel linear map between the platform’s control inputs and applied forces and moments is introduced. The relation between the introduced map and the platform’s ability to hover at different orientations is developed. Correspondingly, the conditions for MRAVs with tiltable propellers to realize and sustain static hovering are detailed. A numerical metric is then introduced, which reflects the ability of MRAVs to sustain static hovering at different orientations. A subclass of MRAVs with tiltable propellers is defined as the critically statically hoverable platforms (CSH), where CSH platforms are MRAVs that cannot sustain static hovering with fixed propellers, but can achieve static hovering with tilting propellers. Finally, extensive simulations are conducted to test and validate the above findings, and to demonstrate the effect of the proposed numerical metric on the platform’s dynamics.

Funder

Khalifa University of Science, Technology and Research

Publisher

ASME International

Subject

Mechanical Engineering

Reference31 articles.

1. Design of a Four-Rotor Aerial Robot;Pounds,2002

2. Fully Actuated Multirotor UAVS: A Literature Review;Rashad;IEEE Rob. Automat. Mag.,2020

3. Design, Modeling and Control of an Omni-Directional Aerial Vehicle;Brescianini,2016

4. Omni-Plus-Seven (O7+): An Omnidirectional Aerial Prototype With a Minimal Number of Unidirectional Thrusters;Hamandi,2020

5. Review of Designs and Flight Control Techniques of Hybrid and Convertible VTOL UAVS;Ducard;Aerosp. Sci. Technol.,2021

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