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van Baelen, D. (author), van Paassen, M.M. (author), Ellerbroek, Joost (author), Abbink, D.A. (author), Mulder, Max (author)
Modern aircraft can be equipped with a flight envelope protection system: automation which modifies pilot control inputs to ensure that the aircraft remains within the allowable limits. Overruling the pilot inputs may lead to mode confusion, even when visual or auditory feedback is provided to alert pilots. We advocate using active control...
journal article 2021
document
van Baelen, D. (author), van Paassen, M.M. (author), Ellerbroek, Joost (author), Abbink, D.A. (author), Mulder, Max (author)
Modern aircraft use a variety of fly-by-wire control devices and combine these with a flight envelope protection system to limit pilot control inputs when approaching the aircraft limits. The current research project aims to increase pilot awareness of such a protection system through the use of force feedback on the control device, i.e.,...
conference paper 2021
document
van Baelen, D. (author), Ellerbroek, Joost (author), van Paassen, M.M. (author), Abbink, D.A. (author), Mulder, Max (author)
Modern aircraft use a variety of fly-by-wire control devices and combine these with a flight envelope protection system to limit pilot control inputs when approaching the aircraft limits. The current research project aims to increase pilot awareness of such a protection system through the use of force feedback on the control device, i.e.,...
conference paper 2020
document
van Baelen, D. (author), Ellerbroek, Joost (author), van Paassen, M.M. (author), Mulder, Max (author)
Several modern aircraft use a passive control manipulator: a spring–damper system that generates command signals to the flight control computers in combination with a flight envelope protection system that limits pilot inputs when approaching the aircraft limits. This research project aims to increase pilot awareness of this protection system...
journal article 2020
document
van Baelen, D. (author), Ellerbroek, Joost (author), van Paassen, M.M. (author), Mulder, Max (author)
Modern fly-by-wire aircraft use flight envelope protection systems, whose actions are not always clear to pilots. To promote situation awareness, proximity to the limits of the flight envelope can be communicated using haptic feedback, by providing forces through the control device. Such a system was developed and this paper reports on the...
conference paper 2019
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van Paassen, M.M. (author), Borst, C. (author), Ellerbroek, Joost (author), Mulder, Max (author), Flach, John M. (author)
Ecological interface design (EID) was originally developed in the context of process control but has been extended into many domains where technology has resulted in both changing work demands and increased opportunities for improved interface applications. This paper gives an overview of the application of the EID to the control of vehicle...
journal article 2018
document
van Baelen, D. (author), Ellerbroek, Joost (author), van Paassen, M.M. (author), Mulder, Max (author)
Current Airbus aircraft use a fly-by-wire control device: a passive spring-damper system which generates, without any force feedback, an electrical signal to the flight control computer. Additionally, a hard flight envelope protection system is used which can limit the inputs of the pilot when approaching the edges of the flight envelope. To...
conference paper 2018
document
Ellerbroek, Joost (author), Rodriguez Martin, M.J.M. (author), Lombaerts, T (author), van Paassen, M.M. (author), Mulder, Max (author)
This paper describes the design and evaluation of a shared control, haptic feedback system to communicate Flight Envelope Protection System intent. The concept uses a combination of stiffness feedback and vibration to communicate proximity of the aircraft state to flight envelope boundaries. In addition, a stick center shift can be applied by...
journal article 2016
document
Ellerbroek, J. (author), Brantegem, K.C.R. (author), Van Paassen, M.M. (author), Mulder, M. (author)
This paper describes a concept for a coplanar airborne self-separation display, which is designed to aid pilots in their separation task, by visualizing the possibilities for conflict resolution that the airspace provides. This study is a part of an ongoing research toward the design of a constraint-based 3-D separation assistance interface that...
journal article 2013
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Ellerbroek, J. (author), Brantegem, K.C.R. (author), Van Paassen, M.M. (author), Mulder, M. (author)
Two experiments, an active conflict resolution task and a passive situation awareness assessment, were conducted that compared two versions of a constraint-based coplanar airborne separation assistance display. A baseline display showed a maneuver space based on 2-D projections of traffic and performance constraints. A second augmented display...
journal article 2013
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Ellerbroek, J. (author), Visser, M. (author), Van Dam, S.B.J. (author), Van Paassen, M.M. (author), Mulder, M. (author)
In the context of the Next Generation Air Transportation System and Single European Sky ATM Research future airspace programs, this paper describes a concept for an airborne separation assurance display that is designed to aid pilots in their task of self-separation, by visualizing the possibilities for conflict resolution that the airspace...
journal article 2011
document
Ellerbroek, J. (author), Stroosma, O. (author), Van Paassen, M.M. (author), Mulder, M. (author)
A set of experiments has been conducted to investigate the relative effect of translational and rotational motion cues on pilot performance. Two helicopter yaw control tasks were performed on the SIMONA: a yaw capture task and a target-tracking task with simulated turbulence. The yaw capture task was a repetition of a task performed previously...
journal article 2008
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