Preliminary study and design of the avionics system for an eVTOL aircraft.

The project consists of the study, creation, implementation, and development of the avionics system of an electric Vertical Take-Off and Landing (eVTOL) airplane for an ongoing project from the company ONAEROSPACE. The plane is intended to be for 7 passengers and 1 pilot, with a maximum range of 1000+ km. The fuselage will be formed of carbon fiber composite to reduce weight and it will use electric motors powered by batteries. The avionics system will provide the aircraft with communication and navigation systems, an autonomous Take-Off (T/O) and landing system, as well as the development of cockpit management systems. This document is divided into two parts. The first part begins with the study of all the necessary tools for communication and navigation systems. That means all compulsory antennas and sensors to obtain information about the surroundings (weather, obstacles, other planes¿). The intern communication network to send data from these sensors and antennas to main flight management systems is also studied in this first part. The second part of the project is dedicated to cabin cockpit systems and the study for the future development of autonomous systems. The cabin will have a full-glass cockpit, with touchable screens and an intelligent voice assistant. It will be very ergonomic and simple, with a lot of space in the cabin. In order to have an idea of the cost of the implementation of all the systems for the aircraft, a weight and cost estimation analysis are done at the end of each section. The last part of the project consists of the study of the design of a virtual intelligent voice assistant and the implementation of autonomous systems. Nowadays, the virtual intelligent voice assistant is an artificial intelligence system that works as a pilot monitoring system which assists the pilot in order to decrease the pilot¿s workload. The future idea is that the pilot could tell commands to the voice assistant and do nothing with the hands, just control that everything works correctly. Regarding the autonomous system, the conclusion is that with the existent technology is not possible today. Nevertheless, in the future, when fully autonomous aircraft are possible, the idea is that although being fully autonomous, the pilot can take the control of the aircraft at any moment.OutgoingObjectius de Desenvolupament Sostenible::9 - Indústria, Innovació i InfraestructuraObjectius de Desenvolupament Sostenible::11 - Ciutats i Comunitats Sostenible

Divergence Between the Human State Assumption and Actual Aircraft System State

Divergence is defined in this thesis as an inconsistency between the human operator’s assumption of the system state and the actual state of the system, which is substantial enough to have consequential effects on the outcome of the situation. The purpose of this thesis is to explore the concept of divergence and develop a framework that can be used to identify the consequential causes of divergence in cases involving human-system interaction. Many recent aircraft accidents involve divergence between the crew state assumption and the actual system state. As aircraft systems and automation become more complex, it’s possible that the consequential effects of divergence, illustrated by these accidents, could become more prevalent due to the correspondingly more complex understanding that may be required by the crew to effectively operate the aircraft. Divergence was explored as a concept by (1) understanding the previous literature related to divergence such as work on human error, human information processing, situation awareness, and mode awareness (2) developing a framework that can be used to understand possible causes of divergence, (3) illustrating use of the framework with accident case studies, and (4) discussing the implications of the findings of the case study analysis of divergence. Human information processing of divergence was developed using the established human information processing literature including Wickens (1992), Endsley (1995), and Reason (1990). The framework highlighted the inputs to the human and represented human processing of this information in relation to formation of a state assumption. The process model was used to identify potential causes of divergence, which were hypothesized as human information processing failures affecting the human state assumption, and to evaluate the effects of those failures on downstream processes and the human state assumption. Eleven accident case studies involving automation mode confusion were conducted to evaluate divergence using the process model of divergence. Eight of the case studies involved auto-throttle mode confusion and the three remaining cases involved divergence in other automation systems that resulted in controlled flight into terrain. The industry implications of the findings of the case studies were then discussed.U.S. Department of Transportation – Federal Aviation Administration through the Joint Universities Program (JUP) FAA 11-G-016 and NASA’s Aeronautics Fellowship Program

A design strategy for human-system integration in aerospace: Where to start and how to design information integration for dynamic, time and safety critical systems

The aim of this research is to develop a framework that provides systemic design guidance for future interfaces that are to provide effective and cognitively suitable information presentation to operators in dynamic and time-critical domains. The aerospace domain has been chosen as the focus for this study. In the aerospace domain there are numerous reported accidents where contributory factors are attributed to pilots’ misunderstanding of automated system configurations, and pilots’ misinterpretation of system behaviour. These problems have occurred as rapid advances in technology have led to an overabundance of ‘useful’ information being presented to the pilot. Currently, the information presented to pilots is often disjointed and distributed across various interfaces where each interface is based on its own design rationale. This creates problems where the pilot either cannot locate information in a timely manner, or misinterprets the available information. There is a need for a systematic design process that deals with meaningfully presenting the abundance of features and interactions of the new technology introduced into the cockpit through the use of existing domain knowledge, structures and strategies drawn from existing pilot training and experience. The thesis is a case study. It shows how a new systematic interface design guidance process was developed by first identifying effective information presentation directly from airforce and airline pilots in their time-critical working environment conducted through observational and empirical studies. The studies provided answers for research questions that were concerned with finding appropriate information presentations for pilots. This resulted in a framework that serves as a guide for the interface designer on how to arrive at, structure and present information to an operator in a cognitively efficient manner. The thesis demonstrates two applications of the design framework, one of which is then evaluated by pilots who demonstrate significantly improved speed and accuracy performance when compared to conventional alphanumerical displays. The applications and limitations of the framework are also discussed.EThOS - Electronic Theses Online ServiceGBUnited Kingdo

Aeronautical Engineering. A continuing bibliography with indexes, supplement 136, June 1981

This bibliography lists 424 reports, articles, and other documents introduced into the NASA scientific and technical information system in May 1981

An Innovative Human Machine Interface for UAS Flight Management System

The thesis is relative to the development of an innovative Human Machine Interface for UAS Flight Management System. In particular, touchscreena have been selected as data entry interface. The thesis has been done together at Alenia Aermacch

Autonomous Approach and Landing Algorithms for Unmanned Aerial Vehicles

In recent years, several research activities have been developed in order to increase the autonomy features in Unmanned Aerial Vehicles (UAVs), to substitute human pilots in dangerous missions or simply in order to execute specific tasks more efficiently and cheaply. In particular, a significant research effort has been devoted to achieve high automation in the landing phase, so as to allow the landing of an aircraft without human intervention, also in presence of severe environmental disturbances. The worldwide research community agrees with the opportunity of the dual use of UAVs (for both military and civil purposes), for this reason it is very important to make the UAVs and their autolanding systems compliant with the actual and future rules and with the procedures regarding autonomous flight in ATM (Air Traffic Management) airspace in addition to the typical military aims of minimizing fuel, space or other important parameters during each autonomous task. Developing autolanding systems with a desired level of reliability, accuracy and safety involves an evolution of all the subsystems related to the guide, navigation and control disciplines. The main drawbacks of the autolanding systems available at the state of art concern or the lack of adaptivity of the trajectory generation and tracking to unpredicted external events, such as varied environmental condition and unexpected threats to avoid, or the missed compliance with the guide lines imposed by certification authorities of the proposed technologies used to get the desired above mentioned adaptivity. During his PhD period the author contributed to the development of an autonomous approach and landing system considering all the indispensable functionalities like: mission automation logic, runway data managing, sensor fusion for optimal estimation of vehicle state, trajectory generation and tracking considering optimality criteria, health management algorithms. In particular the system addressed in this thesis is capable to perform a fully adaptive autonomous landing starting from any point of the three dimensional space. The main novel feature of this algorithm is that it generates on line, with a desired updating rate or at a specified event, the nominal trajectory for the aircraft, based on the actual state of the vehicle and on the desired state at touch down point. Main features of the autolanding system based on the implementation of the proposed algorithm are: on line trajectory re-planning in the landing phase, fully autonomy from remote pilot inputs, weakly instrumented landing runway (without ILS availability), ability to land starting from any point in the space and autonomous management of failures and/or adverse atmospheric conditions, decision-making logic evaluation for key-decisions regarding possible execution of altitude recovery manoeuvre based on the Differential GPS integrity signal and compatible with the functionalities made available by the future GNSS system. All the algorithms developed allow reducing computational tractability of trajectory generation and tracking problems so as to be suitable for real time implementation and to still obtain a feasible (for the vehicle) robust and adaptive trajectory for the UAV. All the activities related to the current study have been conducted at CIRA (Italian Aerospace Research Center) in the framework of the aeronautical TECVOL project whose aim is to develop innovative technologies for the autonomous flight. The autolanding system was developed by the TECVOL team and the author’s contribution to it will be outlined in the thesis. Effectiveness of proposed algorithms has been then evaluated in real flight experiments, using the aeronautical flying demonstrator available at CIRA