The position and attitude tracking of a rigid spacecraft is approached with coupled six-
degrees-of-freedom dynamics described by dual quaternions. By taking advantage of the …

A robust two‐loops structured control system design for quadrotor's position/attitude
trajectory tracking is proposed. The aim of the outer loop is to provide the roll/pitch tilting …

The attitude control problem of a spacecraft using two reaction wheels is revisited.
Controllability analysis shows that the reduced dynamics of a two-wheeled spacecraft are …

The paper investigates the event-triggered sub-optimal control problem for two-time-scale
systems with unknown slow dynamics. Specifically, a composite event-triggered optimal …

This paper presents the two-loops Robust Generalized Dynamic Inversion (RGDI) Quadrotor
control system design. The outer loop of the system provides pitch and roll attitude …

The development of a two-loops Quadrotor's robust generalized dynamic inversion (RGDI)-
based control system is presented. The outer (position) loop utilizes PD position control of …

The nonlinear control problem of aircraft trajectory tracking is tackled in the framework of
multiple linear time-varying constrained control using the newly developed paradigm of …

Generalised dynamic inversion control design methodologies for realisation of linear
spacecraft attitude servo-constraint dynamics is introduced. A prescribed stable linear …

The attitude control of a rigid spacecraft with two skew single-gimbal control moment gyros
(CMGs), which is subject to an underactuated nonholonomic constraint, is investigated …

A unifying methodology is introduced for smooth asymptotic stabilisation of underactuated
rigid body dynamics under one and two degrees of actuation. The methodology is based on …