Nonlinear generalised dynamic inversion for aircraft manoeuvring control

I Hameduddin, AH Bajodah - International Journal of Control, 2012 - Taylor & Francis
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 …

Servo-constraint realization for underactuated mechanical systems

W Blajer, R Seifried, K Kołodziejczyk - Archive of applied mechanics, 2015 - Springer
The paper deals with underactuated mechanical systems, featured by less control inputs m
than degrees of freedom f, m< f, subject to m servo-constraints (specified in time outputs) on …

Flight reconfiguration system–an emergency system of the future

P Grzybowski, E Szpakowska-Peas - Aircraft Engineering and …, 2020 - emerald.com
Purpose This paper aims to describe the idea and partial result of research on flight
reconfiguration system (FRS) which is to be used in case of pilot incapacitation while …

Simulation and testing of flight stabilisation system using trimmers

M Krawczyk, A Zajdel, C Szczepański - Conference on Automation, 2021 - Springer
The main goal of the research presented in this paper is testing the possibility of introducing
the automatic trimming system for the aeroplane flight stabilisation purpose. If successful, it …

The use of servo-constraints in the inverse dynamics analysis of underactuated multibody systems

W Blajer - Journal of Computational and Nonlinear …, 2014 - asmedigitalcollection.asme.org
Underactuated mechanical systems have fewer control inputs than degrees of freedom. The
specified in time outputs, equal in number to the number of inputs, lead to servo-constraints …

Inverse dynamics of underactuated mechanical systems: a simple case study and experimental verification

W Blajer, K Dziewiecki, K Kołodziejczyk… - … in Nonlinear Science and …, 2011 - Elsevier
Underactuated systems are featured by fewer control inputs than the degrees-of-freedom,
m< n. The determination of an input control strategy that forces such a system to complete a …

Coupled differential-algebraic equations framework for modeling six-degree-of-freedom flight dynamics of asymmetric fixed-wing aircraft

OA Marzouk - arXiv preprint arXiv:2412.17280, 2024 - arxiv.org
This study presents a comprehensive mathematical framework for modeling the flight
dynamics of a six-degree-of-freedom fixed-wing aircraft as a rigid body with three control …

Diversity of servo-constraint problems for underactuated mechanical systems: a case study illustration

W Blajer, R Seifried, K Kołodziejczyk - Solid State Phenomena, 2013 - Trans Tech Publ
Underactuated mechanical systems are systems with fewer control inputs than degrees of
freedom. Determination of an input control strategy that forces an underactuated system to …

[图书][B] Specified motion and feedback control of engineering structures with distributed sensors and actuators

A Ghasemi - 2012 - search.proquest.com
This dissertation addresses the control of flexible structures using distributed sensors and
actuators. The objective to determine the required distributed actuation inputs such that the …

Generalized dynamic inversion control for aircraft constrained trajectory tracking applications

I Hameduddin, AH Bajodah - 2012 American Control …, 2012 - ieeexplore.ieee.org
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 …