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 …

Due to the reliance on model knowledge and the lack of compensation mechanism,
Nonlinear Dynamic Inversion (NDI) control does not provide the essential robustness in the …

Inevitable noises and limited computational time are major issues for time-variant matrix
inversion in practice. When designing a time-variant matrix inversion algorithm, it is highly …

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 …

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 aim of this article was to determine control strategy for balance control of rotary double
inverted pendulum system, which is highly nonlinear and unstable under-actuated system …

In this paper, Generalized Dynamic Inversion (GDI) control methodology for linear state
equality constraints is proposed for independent motion control of an aircraft along the roll …