Relevant bibliographies by topics / Helicopter flight operations / Dissertations / Theses
To see the other types of publications on this topic, follow the link: Helicopter flight operations.

Dissertations / Theses on the topic 'Helicopter flight operations'

Author: Grafiati
Published: 6 September 2023

Create a spot-on reference in APA, MLA, Chicago, Harvard, and other styles

Select a source type:

Consult the top 15 dissertations / theses for your research on the topic 'Helicopter flight operations.'

Next to every source in the list of references, there is an 'Add to bibliography' button. Press on it, and we will generate automatically the bibliographic reference to the chosen work in the citation style you need: APA, MLA, Harvard, Chicago, Vancouver, etc.

You can also download the full text of the academic publication as pdf and read online its abstract whenever available in the metadata.

Browse dissertations / theses on a wide variety of disciplines and organise your bibliography correctly.

1

Lentz, Frederick Charles. "Integration of ASW helicopter operations and environment into NPSNET." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1995. http://handle.dtic.mil/100.2/ADA304302.

Full text
Abstract:
Thesis (M.S. in Computer Science) Naval Postgraduate School, September 1995.<br>"September 1995." Thesis advisor(s): Michael J. Zyda, John S. Falby. Includes bibliographical references (p. 107). Also available online.
APA, Harvard, Vancouver, ISO, and other styles
2

Ngo, Tri Dinh. "Constrained Control for Helicopter Shipboard Operations and Moored Ocean Current Turbine Flight Control." Diss., Virginia Tech, 2016. http://hdl.handle.net/10919/71685.

Full text
Abstract:
This dissertation focuses on constrained control of two applications: helicopter and ocean current turbines (OCT). A major contribution in the helicopter application is a novel model predictive control (MPC) framework for helicopter shipboard operations in high demanding sea-based conditions. A complex helicopter-ship dynamics interface has been developed as a system of implicit nonlinear ordinary differential equations to capture essential characteristics of the nonlinear helicopter dynamics, the ship dynamics, and the ship airwake interactions. Various airwake models such as Control Equiva
APA, Harvard, Vancouver, ISO, and other styles
3

Shafer, Daniel Manfred. "Active and Passive Flow Control over the Flight Deck of Small Naval Vessels." Thesis, Virginia Tech, 2005. http://hdl.handle.net/10919/32427.

Full text
Abstract:
Helicopter operations in the vicinity of small naval surface vessels often require excessive pilot workload. Because of the unsteady flow field and large mean velocity gradients, the envelope for flight operations is limited. This experimental investigation uses a 1:144 scale model of the U.S. Navy destroyer DDG-81 to explore the problem. Both active and passive flow control techniques were used to improve the flow field in the helicopterâ s final decent onto the flight deck. Wind tunnel data was collected at a set of grid points over the shipâ s flight deck using a single component hotw
APA, Harvard, Vancouver, ISO, and other styles
4

Pereira, Figueira José Márcio. "The use of offline simulation tools to estimate ship-helicopter operating limitations." Thesis, Aix-Marseille, 2017. http://www.theses.fr/2017AIXM0511/document.

Full text
Abstract:
Les limitations d’atterrissage des hélicoptères ne sont pas valables dans l'environnement à bord d’un navire. Il n'existe aucune méthodologie approuvée de l'analyse ou de la simulation pour évaluer la compatibilité des hélicoptères-navires et préparer les essais de qualification hélicoptères-navires. Dans ce contexte, le présent travail présente le développement et l'analyse d'une méthodologie hors ligne pour déterminer les limites opérationnelles hélicoptères-navires, SHOLs, en fonction des prédictions d’un modèle de pilote humain. Pour cela, des essais pilotés par des humains sont effectués
APA, Harvard, Vancouver, ISO, and other styles
5

DERE, Ahmet Murat. "Flight regime recognition analysis for the army UH-60A IMDS usage." Thesis, Monterey, California. Naval Postgraduate School, 2006. http://hdl.handle.net/10945/2510.

Full text
Abstract:
Approved for public release; distribution is unlimited<br>Usage Monitoring requires accurate regime recognition. For each regime, there is a usage assigned for each component. For example, the damage accumulated at a component is higher if the aircraft is undergoing a high G maneuver than in level flight. The objective of this research is to establish regime recognition models using classification algorithms. The data used in the analysis are the parametric data collected by the onboard system and the actual data, consisting of the correct regime collected from the flight cards. This stud
APA, Harvard, Vancouver, ISO, and other styles
6

Forrest, James Stephen. "Predicting ship-helicopter operating limits using time-accurate CFD ship airwakes and piloted flight simulation." Thesis, University of Liverpool, 2009. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.526869.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

Johnson, Kevin Lee. "Prediction of operational envelope maneuverability effects on rotorcraft design." Diss., Georgia Institute of Technology, 2013. http://hdl.handle.net/1853/47601.

Full text
Abstract:
Military helicopter operations require precise maneuverability characteristics for performance to be determined for the entire helicopter flight envelope. Historically, these maneuverability analyses are combinatorial in nature and involve human-interaction, which hinders their integration into conceptual design. A model formulation that includes the necessary quantitative measures and captures the impact of changing requirements real-time is presented. The formulation is shown to offer a more conservative estimate of maneuverability than traditional energy-based formulations through quantitat
APA, Harvard, Vancouver, ISO, and other styles
8

Revor, Mark S. "An analysis of the integrated mechanical diagnostics health and usage management system on rotor track and balance." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2004. http://library.nps.navy.mil/uhtbin/hyperion/04Jun%5FRevor.pdf.

Full text
Abstract:
Thesis (M.S. in Operations Research)--Naval Postgraduate School, June 2004.<br>Thesis advisor(s): Lyn R. Whitaker, Arnold H. Buss. Includes bibliographical references (p. 77-78). Also available online.
APA, Harvard, Vancouver, ISO, and other styles
9

Unnikrishnan, Suraj. "Adaptive Envelope Protection Methods for Aircraft." Diss., Georgia Institute of Technology, 2006. http://hdl.handle.net/1853/11478.

Full text
Abstract:
Carefree handling refers to the ability of a pilot to operate an aircraft without the need to continuously monitor aircraft operating limits. At the heart of all carefree handling or maneuvering systems, also referred to as envelope protection systems, are algorithms and methods for predicting future limit violations. Recently, envelope protection methods that have gained more acceptance, translate limit proximity information to its equivalent in the control channel. Envelope protection algorithms either use very small prediction horizon or are static methods with no capability to adapt to cha
APA, Harvard, Vancouver, ISO, and other styles
10

Praveen, B. "Study of the ship airwake-helodeck flow field for safe helo operations." Thesis, 2018. http://localhost:8080/xmlui/handle/12345678/7776.

Full text
APA, Harvard, Vancouver, ISO, and other styles
11

Yang, Tzu-Chien, and 楊子健. "A Study on New Attack Helicopter with Unmanned Flight Vehicle System in Anti-landing Operations." Thesis, 2019. http://ndltd.ncl.edu.tw/handle/fy45zy.

Full text
Abstract:
碩士<br>崑山科技大學<br>資訊管理研究所<br>107<br>With the modernization of the Armed Forces in China, the CCP's technology is developing rapidly by the along of economic growth recently. Consequently, its weapons and equipments were evolving with each passing day. No matter from information, missiles, and space technology, it is far superior compared to the armed force. Especially, the CCP accelerated the missile's ability to project capability with the high precision after the Gulf War. The ability to anti-missile is an important part of high-tech for long-distance missile projection. In response to the mil
APA, Harvard, Vancouver, ISO, and other styles
12

Sung, Le-Yeh, and 宋樂業. "Human Factors Analysis for Helicopter Flight Operation." Thesis, 2006. http://ndltd.ncl.edu.tw/handle/76695435579766537165.

Full text
Abstract:
碩士<br>國立成功大學<br>高階管理碩士在職專班<br>94<br>In the passed decade, the average accident rate is approximately 1.66 mishaps per million flight hours for the Republic of China (ROC) civil aircraft and it is 3.07 times of the World's average --- 0.54 mishaps per million flight hours. In addition, the average accident rate is 34.08 mishaps per 100,000 flight hours for the ROC rotor-wing aircraft while it is 8.74 for the USA rotor-wing aircraft. The ROC helicopter accident rate is almost 4 times of the USA accident rate. According to the data I mentioned above, the ROC flight safety is a concern when it is
APA, Harvard, Vancouver, ISO, and other styles
13

Su, Yinyi, and 蘇殷逸. "Numerical Investigation on Influence of Engine Exhaust on Flight Operation of Shipboard Helicopter." Thesis, 2011. http://ndltd.ncl.edu.tw/handle/42465699817330907929.

Full text
Abstract:
碩士<br>國防大學理工學院<br>造船及海洋工程碩士班<br>99<br>The exhausted gases from ships upper smoke are corrosive. They will erode and pollute the equipments on the deck, harm the people’s health on the ship deck, even threat the flight crew’s safety. So, predicting the plume trajectory is necessary and helpful. The factors influent the plume flow are numerous and complicated, such as wind velocity, exhausted gases velocity from the plume, the plume temperature, the plume height, the front structures, and so on, all of them will affect the gases flow. For preventing the gases create damage, we need to make desig
APA, Harvard, Vancouver, ISO, and other styles
14

Kuo-MingChu and 朱國明. "Analysis of Digital to Analog Flight Instruments in Helicopter Cockpit Against Pilot’s Operation Margin." Thesis, 2013. http://ndltd.ncl.edu.tw/handle/73010238147679945232.

Full text
Abstract:
碩士<br>國立成功大學<br>航空太空工程學系專班<br>101<br>In the process of aviation evolution, the structure of airframe, composite materials and the power technology improve persistently. The primary goal of all these improvement was to speed up the aircraft, increase the flight altitude, extend travel distance, and expand the carrying capacity. Nevertheless, the complexity of aviation system has been influencing pilot's aircraft manipulation. Statistics showed, according to ICAO, that more than 70 percent of aircraft accidents directly or indirectly related to incorrect pilot manipulation. Therefore, the modern
APA, Harvard, Vancouver, ISO, and other styles
15

Wei, Hwang Jyh, and 黃志偉. "A Study on the Safe Operating Envelopes of a Helicopter/Ship Landing Set by Flight Qualities." Thesis, 2006. http://ndltd.ncl.edu.tw/handle/59744187163557853388.

Full text
Abstract:
碩士<br>國防大學中正理工學院<br>兵器系統工程研究所<br>94<br>In this thesis, the investigation of onboard helicopter flight safe operating envelopes in different kinds of sea conditions set by flying qualities during landing are of particular interest. This thesis includes five key steps: Firstly, incorporating the six degree-of-freedom equations of motion and the steady-state airwake on the flight deck, the helicopter/ship recovery model is established. Second, we analyse the influence of ship speed and wave cycle to the ship motions in different kinds of sea conditions. Third, three kinds of controller are design
APA, Harvard, Vancouver, ISO, and other styles
We offer discounts on all premium plans for authors whose works are included in thematic literature selections. Contact us to get a unique promo code!

To the bibliography