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Design of a retrofitted pilot-controlled system to conduct flight-deck interval management (本文)

Riedel, Timo Mario 慶應義塾大学

2020.03.23

概要

This thesis explores Flight-deck Interval Management (FIM), an airborne self-spacing technology to ensure the safe and efficient operation of aircraft in highly utilized airspace by speed control. Leading research on FIM was conducted by the National Aeronautics and Space Administration (NASA), who proposed the current control logic ASTAR, and designed the dedicated avionics for FIM. However, industry demand and the wish to demonstrate the technology earlier called for a paradigm change from a fully automated, to a retrofitted, pilot-controlled system. In early 2017, NASA concluded their research on FIM with a flight test that revealed that the current control logic issues too many speed commands, and thereby causes too much workload for the pilots. Therefore, it was recommended to explore alternative control logics to achieve operational implementation.

The aim and originality of this thesis is in the proposal, optimization, and testing of a new, easy- to-integrate control logic, called IM-SP, that uses an original two-staged rule-based speed plan modification concept, which employs performance and pilot workload related decision factors. Focus was given on the reduction of speed commands and other findings made by NASA during their test. Optimization was achieved using evolutionary algorithms, and a flight simulator evaluation, involving airline and test pilots, was conducted. It is envisioned that the results of this thesis will provide the FIM research community with tools and ideas to bring FIM toward operational implementation, so that the time and performance goals of global and national airspace improvement initiatives are met.

Chapter 1 introduces the current research matter, motivation for the topic, and the thesis structure.

Chapter 2 explains the concepts and history of FIM in further detail and gives a description of the ASTAR control logic along an in-depth analysis of the issues found in the ATD-1 flight test. Further, other models and concepts important to this thesis are presented.

Chapter 3 shows the research results of multiple feasibility studies using large-scale Monte Carlo simulations of aircraft using ASTAR based FIM on arrivals in Tokyo International Airport. These simulations were used to investigate the spacing performance and speed control behavior of ASTAR and to ensure arrival route compatibility under local environmental conditions.

Chapter 4 introduces the IM-SP concept and describes its design principles and two-staged selection-algorithm. Two benchmark studies are shown, comparing the performance of ASTAR to IM-SP.

Chapter 5 describes an optimization study of IM-SP, using Particle Swarm Optimization to improve the selection logic for an improved spacing performance, user friendliness and ecology. Two distinctive results, a spacing performance optimal, and a fuel performance improved solution, are shown in detail.

Chapter 6 presents the setup and results of the flight simulator evaluation in which airline and certified test pilots evaluated FIM, ASTAR and IM-SP in an Airbus A320 flight simulator, recreating the ATD-1 flight test environment. Pilots’ comments are provided and further observations are presented

Chapter 7 concludes this paper with a summary of the research achievements and an outlook on future research tasks, including potential enhancements for FIM.

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