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Dissertations / Theses on the topic 'Landing phase'

Author: Grafiati

Published: 30 May 2022

Last updated: 31 July 2025

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1

Wellons, William Lee. "A shipboard global positioning system carrier phase interferometric aircraft flight reference system." Ohio : Ohio University, 1994. http://www.ohiolink.edu/etd/view.cgi?ohiou1179860957.

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2

Volný, Michael. "Reactive and soft landing of polyatomic gas-phase ions on plasma-treated metal surfaces /." Thesis, Connect to this title online; UW restricted, 2006. http://hdl.handle.net/1773/8650.

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3

Yildiz, Guray. "Dynamic Approach To Wind Sensitive Optimum Cruise Phase Flight Planning." Master's thesis, METU, 2012. http://etd.lib.metu.edu.tr/upload/12615098/index.pdf.

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A Flight Management System (FMS) performs 4 Dimensional flight planning<br>Lateral Planning (Calculation of the latitude and longitudes of waypoints), Vertical Planning (Calculation of the altitudes of waypoints) and Temporal Planning(Calculation of Estimated Time of Arrival). Correct and accurate calculation of4D flight path and then guiding the pilot/airplane to track the route in specified accuracy limits in terms of lateral (i.e Required Navigational Performance RNP), vertical (Reduced Vertical Seperation Minima RVSM), and time (Required Time of Arrival RTA) is what FMS performs in brief.

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4

Lee, Kyongsun. "Effects of flight factors on pilot performance, workload, and stress at final approach to landing phase of flight." Doctoral diss., University of Central Florida, 2010. http://digital.library.ucf.edu/cdm/ref/collection/ETD/id/4564.

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Similarly, the levels of a gliding angle showed the statistical difference on the performance, workload, and stress (HRV, TLX, and LP: all are p less than] .05). During the flight with 4.5 degree, the pilots showed lower performance with higher workload and stress. However, the levels of the flight experience did not have any influence on the performance, workload, and stress levels (AGPTP, LP, TLX, HRV: all are p greater than] .05). In conclusion, flying in Populated area and flying with a 4.5 degree gliding angle increases the workload and stress level of the pilots. In addition, when the pi

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5

Благая, Людмила Володимирівна, та Liudmyla V. Blahaia. "Модель функціонування системи «пілот–літак» при управлінні рухом на етапі посадки". Thesis, Національний авіаційний університет, 2021. https://er.nau.edu.ua/handle/NAU/52288.

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Розроблено стохастичну математичну модель діяльності ергатичної системи «пілот-літак» на етапі заходу на посадку як системи масового обслуговування, яка об’єднує модельні уявлення станів людини-оператора і технічної частини системи в єдину модель. Результати розробленого програмного забезпечення показали, що параметри, отримані за моделлю, відповідають параметрам польоту, отриманим з системи реєстрації параметрів літака на режимі заходу на посадку. Результати удосконалення математичної моделі «Узагальнена робоча характеристика людини-оператора» дали змогу досліджувати системні характеристики

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6

Ravetta, Patricio A. "LORE Approach for Phased Array Measurements and Noise Control of Landing Gears." Diss., Virginia Tech, 2005. http://hdl.handle.net/10919/29975.

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A novel concept in noise control devices for landing gears is presented. These devices consist of elastic membranes creating a fairing around the major noise sources. The purpose of these devices is to reduce wake interactions and to hide components from the flow, thus, reducing the noise emission. The design of these fairings was focused on the major noise sources identified in a 777 main landing gear. To find the major noise sources, an extensive noise source identification process was performed using phased arrays. To this end, phased array technologies were developed and a 26%-scale 777 ma

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7

Puumala, Rodney. "Ski jumping flight, a kinematic analysis of the mid-flight and preparation for landing phases." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1998. http://www.collectionscanada.ca/obj/s4/f2/dsk1/tape11/PQDD_0025/MQ52073.pdf.

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8

Remillieux, Marcel Christophe. "Aeroacoustic Study of a Model-Scale Landing Gear in a Semi-Anechoic Wind Tunnel." Thesis, Virginia Tech, 2007. http://hdl.handle.net/10919/31674.

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An aeroacoustic study was conducted on a 26%-scale Boeing 777 main landing gear in the Virginia Tech (VT) Anechoic Stability Wind Tunnel. The VT Anechoic Stability Wind Tunnel allowed noise measurements to be carried out using both a 63-elements microphone phased array and a linear array of 15 microphones. The noise sources were identified from the flyover view under various flow speeds and the phased array positioned in both the near and far-field. The directivity pattern of the landing gear was determined using the linear array of microphones. The effectiveness of 4 passive noise control

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9

Bouchouireb, Hamza. "Identification and modelling of noise sources on a realisticnose landing gear using phased array methods applied tocomputational data." Thesis, KTH, MWL Marcus Wallenberg Laboratoriet, 2017. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-209186.

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Due to the recent development of quieter turbofan engines, airframe noise has started to emerge asthe most important noise source. This is particularly true during the approach/landing phase, whenthe engines are operated at low-thrust levels. In order to meet future noise level regulations, thecharacterization and subsequent reduction of landing gear induced noise is necessary. Wind-tunnelaeroacoustic tests have always been the favoured method for assessing and studying the noise generatedby landing gears, but their prohibitive cost has steered the attention towards numerical methods.Since dir

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10

Chuang, Sheng-Wei, and 莊聖維. "Different types of Brace Worn on Biomechanical Analysis During Landing Phase." Thesis, 2010. http://ndltd.ncl.edu.tw/handle/89765276797341663409.

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碩士<br>國立臺北教育大學<br>體育學系碩士班<br>98<br>OBJECTIVES: To investigate involvement of different brace during landing phase on the Kinematic and kinetic parameters. Methods: Eight healthy without any history of lower limb pain of adult men (age 18.5 ± 0.47 years, height 177.63 ± 5.99 cm, weight 66.5 ± 3.12 kg) for the study. A Mega Speed Ms30k high-speed camera (100Hz), An AMTI force platform (1000Hz), Biovision EMG apparatus (1000Hz) and 50g dual-axis accelerometer. Synchronous capture landing phase motion data, and analysis parameters for the buffer period. Video motion analysis software to Kwon3D pro

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11

Lin, Jing-Hsyuan, and 林敬軒. "An Investigation of Flight Data via Modern Analysis Methods for Civil Transport During Landing Phase." Thesis, 2014. http://ndltd.ncl.edu.tw/handle/34061424713938455226.

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碩士<br>淡江大學<br>航空太空工程學系碩士班<br>102<br>In this research, three flight data of Boeing747-400 including two normal and one abnormal are analyzed, which derived from Flight Operations Quality Assurance (FOQA), by using Wavelet Transform and Hilbert-Huang Transform methods. Considering the tremendous amount of relevant parameters involved, such as true airspeed, vertical speed, thrust, angle of attack, wind speed, wind direction, etc., we need to first decompose these engineering data to different frequencies inside the signals, observe their changes, and acquire valuable and meaningful flight interp

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12

Hsu, Yen-Chuan, and 許炎泉. "The Difference between Pilot’s Stress Workload and Personality Trait during Landing Phase with Flight Simulator." Thesis, 2006. http://ndltd.ncl.edu.tw/handle/30827478728356191102.

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碩士<br>國立成功大學<br>工業與資訊管理學系專班<br>94<br>Flight is the three-dimensional motion which differs from human normal movement. It must monitor the environment changing and complex flight control system in all the time. The pilot experienced lots of mental workload in the routine flight. Upon emergency situation, the load became more and more. If the pilot could not handle properly, it would cause the flight accident. The domestic and foreign statistic data indicated that landing is the major phase which occurs an accident during the flight. So, the purpose in this study is to research 1) the pilot enco

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13

(9762467), Pei Su. "Preparative Mass Spectrometry: Instrumentation and Applications." Thesis, 2020.

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<p>Ion soft landing is a preparative mass spectrometry technique that enables intact deposition of polyatomic ions onto surfaces. The ability to select ions with well-defined mass, charge, and kinetic energy, along with precise control over size, shape, and position of the ion beam in the deposition process distinguishes ion soft landing from traditional synthetic and surface preparation approaches. A wide range of projectile ions including molecular ions, non-covalent complexes, clusters, and ionic fragments generated in the gas phase have been used in soft-landing studies to address both th

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14

Wei-ChihYang and 楊偉志. "The Civil Transport Aircraft Performance Analysis in Landing and Taxing Phases under Weather Hazard." Thesis, 2010. http://ndltd.ncl.edu.tw/handle/67975838776845794545.

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碩士<br>國立成功大學<br>航空太空工程學系碩博士班<br>98<br>According to one of published statistics from Boeing Commercial Airplane, there are 50 % of flight accidents that are occurred in landing phase. The weather hazard becomes much more severe when airplanes encounter a strong cross wind. The research aims to infer flight information especially in cross wind effect. The study presents data processing approaches to obtain flight information from actual flight data recorder (FDR) data. Firstly, the Extended Kalman Filter (EKF) is applied to reduce the effect of the data noise and bias of the recorded flight data

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15

Wang, Zion, and 汪錫恩. "A Study of Relative Risk Comparison on Runway Length of Major Airports in Taiwan Influencing the Flight Safety during Take-off and Landing Phases." Thesis, 2008. http://ndltd.ncl.edu.tw/handle/43777670667922928672.

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碩士<br>國立成功大學<br>交通管理學系碩博士班<br>96<br>Runway overrun and excursion have always been the major causes of aircraft accidents during landing and take-off phases. According to the statistics of ASC, these types of accidents shared 8 out of 29 domestic accidents during 1997-2006, the highest number among all types of accidents. In order to improve the worldwide flight safety, ICAO emphasizes not only on preventing human errors and system failures but also on improving the safety of airports and air traffic services, which enlarge the conception of system safety from human, software, and hardware fact

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