Attitude control of a satellite having only two reaction wheels is a challenging issue. To
address this problem, previously published researches considered some simplifying …

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 …

Feasibility of achieving 3-axis stabilization of an asymmetric spacecraft for cases where
there is no control available in one axis (underactuated spacecraft) is explored in this paper …

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 …

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 …

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 …

Underactuated attitude control is supposed to be used on spacecraft when failure happens
with onboard actuators. One main problem with existing underactuated attitude control …

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