The novelty of the proposed work lies in the control technique, referred to as the robust
generalized dynamic inversion based adaptive recursive sliding mode control (RGDI …

The complex structured systems always demand efficient optimization to tackle all problems
(constraints, parametric perturbation, multiobjective due to conflict of design), which must be …

This work is used to design a novel robust optimization control law augmented with Robust
Generalized Dynamic Inversion (RGDI) for continuous varying perturbations in the Twin …

Analyzing the flight quality of an aircraft obliges the examination of the natural stability of the
system. In this paper, the frequency domain response of the F-16 aircraft dynamics is …

This paper presents a new framework for robust relative position and velocity estimation of
satellite formations in Low Earth Orbit (LEO) in the presence of statistical outliers in sensor …

This paper develops a constrained Model Predictive Control (MPC) formulation for
longitudinal control of a fixed wing aircraft. In order to account for the inherent coupling …

This study deals with the problem of stabilizing spatial motion of a maneuverable aircraft
with three controls and nine state parameters. In the task it is required to provide specified …

The successive generalized dynamic inversion (SGDI) control design methodology is used
to control the linearized underactuated three degrees of freedom lateral motion of the F-16 …

The concept of mutual direct linear state controllability (MDC) is introduced for
underactuated mechanical and aerospace systems. The MDC analysis identifies the sets of …

In this paper, a novel Generalized Dynamic Inversion with Sliding Mode Control (GDI-SMC)
approach is developed for the position control of the well known Twin Rotor Multiple-Input …