This paper reviews the effect of multirotor aerial vehicle designs on their abilities in terms of
tasks and system properties. We propose a general taxonomy to characterize and describe …

For the fault tolerant control of an eight-rotor VTOL Unmanned Air Vehicle (UAV), a control
allocation scheme is proposed. The eight-rotor configuration provides actuator redundancy …

We introduce an original configuration of a multi rotor helicopter composed of eight rotors.
Four rotors, also called main rotors, are used to stabilize the attitude of the helicopter, while …

The goal of this paper is to present a novel configuration for a three-rotor mini unmanned
aerial vehicle (UAV). The proposed design incorporates advantageous structural features …

This article proposed a new fixed-time trajectory tracking control strategy based on the
disturbance observer (DOB) for a tilt trirotor unmanned aerial vehicle (TTUAV), which is …

The design, dynamics, and control allocation of tri-rotor unmanned aerial vehicles (UAVs)
are introduced in this paper. A trirotor UAV has three rotor axes that are equidistant from its …

This article focuses on the attitude and altitude tracking control of the tilt trirotor unmanned
aerial vehicle (UAV) which is subject to modeling uncertainties and unknown external …

UNMANNED aerial vehicles (UAVs) have attracted significant attention in recent years for
both military and civilian applications. Among the different configurations of UAVs, those …

In this paper, design, dynamics and control allocation of Tri-Rotor UAV are introduced. Tri-
Rotor UAV has three rotor axes that are equidistant from its center of gravity. There are two …

This paper has implemented nonlinear control strategy for the single tilt tri‐rotor aerial robot.
Based on Newton‐Euler's laws, the linear and nonlinear mathematical models of tri‐rotor …