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 …
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 …
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 …
reconfiguration system (FRS) which is to be used in case of pilot incapacitation while …
Simulation and testing of flight stabilisation system using trimmers
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 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 …
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 …
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 …
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 …
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 …
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 …
multiple linear time-varying constrained control using the newly developed paradigm of …