This paper presents the development of 6-degrees-of-freedom (6-DOF) flight dynamics
model and nonlinear control design for a novel hybrid biplane-quadrotor unmanned aerial …

This paper discusses the conceptual design and proof-of-concept flight demonstration of a
novel variable pitch quadrotor biplane Unmanned Aerial Vehicle concept for payload …

Autonomous landing is a challenging phase of flight for an aerial vehicle, especially when
attempting to land on a moving target. This paper presents vision-based tracking and …

The conceptual design and flight controller of a novel kind of quadcopter are presented. This
design is capable of morphing the shape of the UAV during flight to achieve position and …

In this paper, we present an autonomous flight controller for a quadcopter with thrust
vectoring capabilities. This UAV falls in the category of multirotors with tilt-motion enabled …

In this paper, we present a novel developmental reinforcement learning-based controller for
a quadcopter with thrust vectoring capabilities. This multirotor UAV design has tilt-enabled …

This paper proposes a new mathematical model to map the rotational speed and angle of
attack (pitch) of small-size propellers typically used in multirotors and the aerodynamic thrust …

Quadrotors have enormous application in the area of automated delivery systems. In such
scenarios, payload can vary with time, and cannot be tackled by traditional controllers. This …

Purpose This paper aims to describe the characteristics and modeling of the variable pitch
quadrotor. In a variable pitch quadrotor, unlike ordinary quadrotors that the force is …

In this paper, a robust trajectory tracking control design of a variable-pitch quadrotor (VPQ)
under the adverse conditions of external disturbance and parametric uncertainties is …