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 …

An adaptive controller which is designed with a priori consideration of actuator saturation
effects and guarantees H∞ tracking performance for a class of multiple-input–multiple …

Purpose To design a robust attitude control system for the ascent flight phase of satellite
launch vehicles (SLVs). Design/methodology/approach The autopilot is based on …

A novel two-loop structured robust generalized dynamic inversion–based control system is
proposed for autonomous underwater vehicles. The outer (position) loop of the generalized …

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 …

Abstract The Robust Generalized Dynamic Inversion (RGDI) homing guidance (HG) and
control design methodology is proposed for intercepting highly maneuvering targets. The …

This paper presents the Robust Generalized Dynamic Inversion (RGDI) control system for
Autonomous Underwater Vehicles (AUV) s. The outer (position) and the inner (attitude) …

A novel Generalized Dynamic Inversion (GDI) based two-loops structured control system is
proposed for position and attitude control of Autonomous Underwater Vehicles (AUVs). The …