Attitude stabilization of a VTOL quadrotor aircraft
A Tayebi, S McGilvray - IEEE Transactions on control systems …, 2006 - ieeexplore.ieee.org
In this paper, we propose a new quaternion-based feedback control scheme for exponential
attitude stabilization of a four-rotor vertical takeoff and landing aerial robot known as a …
attitude stabilization of a four-rotor vertical takeoff and landing aerial robot known as a …
Super twisting control algorithm for the attitude tracking of a four rotors UAV
This paper deals with the design and implementation of a nonlinear control algorithm for the
attitude tracking of a four-rotor helicopter known as quadrotor. This algorithm is based on the …
attitude tracking of a four-rotor helicopter known as quadrotor. This algorithm is based on the …
Attitude stabilization of a four-rotor aerial robot
A Tayebi, S McGilvray - … 43rd IEEE conference on decision and …, 2004 - ieeexplore.ieee.org
In this paper, we propose a quaternion-based feedback control scheme for exponential
attitude stabilization of a four-rotor vertical take-off and landing (VTOL) aerial robot known as …
attitude stabilization of a four-rotor vertical take-off and landing (VTOL) aerial robot known as …
Spacecraft attitude control using magnetic actuators
The problem of inertial pointing for a spacecraft with magnetic actuators is addressed and an
almost global solution to the problem is obtained by means of static attitude and rate …
almost global solution to the problem is obtained by means of static attitude and rate …
Position and attitude tracking of AUV's: a quaternion feedback approach
A position and attitude tracking control law for autonomous underwater vehicles (AUV's) in 6
degrees of freedom (DOF) is derived. The 4-parameter unit quaternion (Euler parameters) is …
degrees of freedom (DOF) is derived. The 4-parameter unit quaternion (Euler parameters) is …
Nonlinear H/sub/spl infin//control and its application to rigid spacecraft
W Kang - IEEE Transactions on Automatic Control, 1995 - ieeexplore.ieee.org
The problem of H/sub/spl infin//control of a rigid spacecraft with three control torques and
disturbances is addressed. The Hamilton-Jacobi-Isaacs inequality for H/sub/spl …
disturbances is addressed. The Hamilton-Jacobi-Isaacs inequality for H/sub/spl …
Super twisting control algorithm for the four rotors helicopter attitude tracking problem
This paper deals with the design and implementation of the super twisting control algorithm
for the attitude tracking of a four rotors helicopter known as quadrotor. The choice of this …
for the attitude tracking of a four rotors helicopter known as quadrotor. The choice of this …
Magnetocoulombic attitude control of Earth-pointing satellites
DK Giri, M Sinha - Journal of Guidance, Control, and Dynamics, 2014 - arc.aiaa.org
A magnetocoulombic satellite system is proposed and equations are developed to study the
stability and control characteristics for a set of given initial conditions. An equation for charge …
stability and control characteristics for a set of given initial conditions. An equation for charge …
A Recursive Approach for Magnetic Field Estimation in Spacecraft Magnetic Attitude Control
This paper is concerned with magnetic attitude control of spacecraft. The operation of the
magnetic actuators is usually on a duty cycle; during the off times in this duty cycle the …
magnetic actuators is usually on a duty cycle; during the off times in this duty cycle the …
[PDF][PDF] A coupled estimation and control analysis for attitude stabilisation of mini aerial vehicles
Commercially viable aerial robotic vehicles require robust and efficient, but low-cost attitude
(vehicle orientation) stabilisation systems. A typical attitude stabilisation system employs a …
(vehicle orientation) stabilisation systems. A typical attitude stabilisation system employs a …