Relevant bibliographies by topics / Drone aircraft. Reliability (Engineering)

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers

Academic literature on the topic 'Drone aircraft. Reliability (Engineering)'

Author: Grafiati
Published: 4 June 2021
Last updated: 1 February 2022

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

Select a source type:

Consult the lists of relevant articles, books, theses, conference reports, and other scholarly sources on the topic 'Drone aircraft. Reliability (Engineering).'

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.

Journal articles on the topic "Drone aircraft. Reliability (Engineering)"

1

Kharchenko, V., M. Yastrebenetsky, H. Fesenko, A. Sachenko, and V. Kochan. "NPP Post-Accident Monitoring System Based on Unmanned Aircraft Vehicle: Reliability Models." Nuclear and Radiation Safety, no. 4(76) (November 17, 2017): 50–55. http://dx.doi.org/10.32918/nrs.2017.4(76).08.

Full text
Abstract:
The paper presents various options for the design of NPP post-accident monitoring systems based on drone fleets. Reliability block diagrams of such options are built and formulas for estimating their probability of failure-free operation are obtained. The possibilities of using the developed models for studying the considered system options are shown. An approach to determine the optimal composition of drone fleets for NPP monitoring under restrictions on their flight trajectories is proposed.
APA, Harvard, Vancouver, ISO, and other styles
2

Shafiee, Mahmood, Zeyu Zhou, Luyao Mei, Fateme Dinmohammadi, Jackson Karama, and David Flynn. "Unmanned Aerial Drones for Inspection of Offshore Wind Turbines: A Mission-Critical Failure Analysis." Robotics 10, no. 1 (2021): 26. http://dx.doi.org/10.3390/robotics10010026.

Full text
Abstract:
With increasing global investment in offshore wind energy and rapid deployment of wind power technologies in deep water hazardous environments, the in-service inspection of wind turbines and their related infrastructure plays an important role in the safe and efficient operation of wind farm fleets. The use of unmanned aerial vehicle (UAV) and remotely piloted aircraft (RPA)—commonly known as “drones”—for remote inspection of wind energy infrastructure has received a great deal of attention in recent years. Drones have significant potential to reduce not only the number of times that personnel
APA, Harvard, Vancouver, ISO, and other styles
3

D’Amato, Egidio, Vito Antonio Nardi, Immacolata Notaro, and Valerio Scordamaglia. "A Particle Filtering Approach for Fault Detection and Isolation of UAV IMU Sensors: Design, Implementation and Sensitivity Analysis." Sensors 21, no. 9 (2021): 3066. http://dx.doi.org/10.3390/s21093066.

Full text
Abstract:
Sensor fault detection and isolation (SFDI) is a fundamental topic in unmanned aerial vehicle (UAV) development, where attitude estimation plays a key role in flight control systems and its accuracy is crucial for UAV reliability. In commercial drones with low maximum take-off weights, typical redundant architectures, based on triplex, can represent a strong limitation in UAV payload capabilities. This paper proposes an FDI algorithm for low-cost multi-rotor drones equipped with duplex sensor architecture. Here, attitude estimation involves two 9-DoF inertial measurement units (IMUs) including
APA, Harvard, Vancouver, ISO, and other styles
4

Sibilli, Thierry, Capucine Senne, Hugo Jouan, Askin T. Isikveren, and Sabrina Ayat. "Synergistic hybrid-electric liquid natural gas drone: S.H.I.E.L.D." Aircraft Engineering and Aerospace Technology 92, no. 5 (2020): 757–68. http://dx.doi.org/10.1108/aeat-10-2019-0211.

Full text
Abstract:
Purpose With the objective to assess potentially performant hybrid-electric architectures, this paper aims to present an aircraft performance level evaluation, in terms of range and payload, of the synergies between a hybrid-electric energy system configuration and a cryogenic fuel system. Design/methodology/approach An unmanned aerial vehicle (UAV) is modeled using an aircraft performance tool, modified to take into account the hybrid nature of the system. The fuel and thermal management systems are modeled looking to maximize the synergistic effects. The electrical system is defined in serie
APA, Harvard, Vancouver, ISO, and other styles
5

Brown, Alan S. "The Drone Warriors." Mechanical Engineering 132, no. 01 (2010): 22–27. http://dx.doi.org/10.1115/1.2010-jan-1.

Full text
Abstract:
This article explores the role of robots in military operations in the coming future and challenges posed by it. Military personnel believe that robots may not replace soldiers; however, as automated systems become more capable, they will certainly supplement human troops. On the ground, soldiers deploy robots to search dangerous locations, and to find and defuse roadside bombs. New models that carry weapons have already entered service. Robotic warfare is open-source warfare; enemies cannot only probe robots for technological vulnerabilities, but they can also build robots themselves. Some co
APA, Harvard, Vancouver, ISO, and other styles
6

Gardner, P., and C. R. Day. "Options for Control and Navigation of Unmanned Aircraft." Journal of Navigation 45, no. 3 (1992): 352–68. http://dx.doi.org/10.1017/s0373463300010936.

Full text
Abstract:
Whilst unmanned aircraft (UMA) can be said to encompass missiles, targets for weapon training, preprogrammed reconnaissance drones and civilian systems such as radio-controlled models used to carry cameras, for the purpose of this paper we will restrict ourselves to aircraft which are capable of sustaining autonomous flight and accepting navigation commands whilst airborne. The terms applied to unmanned aircraft are variously UMA, remotely piloted vehicle (RPV), Drone and Unmanned Aerial Vehicle (UAV).
APA, Harvard, Vancouver, ISO, and other styles
7

Newsom, Jerry R., Anthony S. Pototzky, and Irving Abel. "Design of a flutter suppression system for an experimental drone aircraft." Journal of Aircraft 22, no. 5 (1985): 380–86. http://dx.doi.org/10.2514/3.45135.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Lu, Xiaohua, Xinchao Liu, Yingchun Zhang, Yulong Li, and Hongfu Zuo. "Simulation of airborne collision between a drone and an aircraft nose." Aerospace Science and Technology 118 (November 2021): 107078. http://dx.doi.org/10.1016/j.ast.2021.107078.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

SAINTIS, LAURENT, EMMANUEL HUGUES, CHRISTIAN BES, and MARCEL MONGEAU. "COMPUTING IN-SERVICE AIRCRAFT RELIABILITY." International Journal of Reliability, Quality and Safety Engineering 16, no. 02 (2009): 91–116. http://dx.doi.org/10.1142/s0218539309003319.

Full text
Abstract:
This paper deals with the modeling and computation of in-service aircraft reliability at the preliminary design stage. This problem is crucial for aircraft designers because it enables them to evaluate in-service interruption rates, in view of designing the system and of optimizing aircraft support. In the context of a sequence of flight cycles, standard reliability methods are not computationally conceivable with respect to industrial timing constraints. In this paper, first we construct the mathematical framework of in-service aircraft reliability. Second, we use this model in order to demon
APA, Harvard, Vancouver, ISO, and other styles
10

Oosedo, Atsushi, Hiroaki Hattori, Ippei Yasui, and Kenya Harada. "Unmanned Aircraft System Traffic Management (UTM) Simulation of Drone Delivery Models in 2030 Japan." Journal of Robotics and Mechatronics 33, no. 2 (2021): 348–62. http://dx.doi.org/10.20965/jrm.2021.p0348.

Full text
Abstract:
An unmanned aircraft system traffic management (UTM) system to support flights beyond visual line-of-sight is considered necessary for the promotion of commercial drone use. In the research and development of UTM systems, cost and time constraints make it difficult to actually fly a large number of drones in the same airspace, so research is mainly conducted using a simulator. This paper presents details of a UTM simulator named the “scalable simulator for knowledge of low-altitude environment” (SKALE) developed by the Japan Aerospace Exploration Agency (JAXA), with respect to the construction
APA, Harvard, Vancouver, ISO, and other styles
More sources

Dissertations / Theses on the topic "Drone aircraft. Reliability (Engineering)"

1

Dermentzoudis, Marinos. "Establishment of models and data tracking for small UAV reliability." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2004. http://library.nps.navy.mil/uhtbin/hyperion/04Jun%5FDermentzoudis.pdf.

Full text
Abstract:
Thesis (M.S. in Operations Research and M.S. in Systems Engineering)--Naval Postgraduate School, June 2004.<br>Thesis advisor(s): David Olwell. Includes bibliographical references (p. 217-224). Also available online.
APA, Harvard, Vancouver, ISO, and other styles
2

Venter, Jacob. "Development of an experimental tilt-wing VTOL unmanned aerial vehicle." Thesis, Link to the online version, 2006. http://hdl.handle.net/10019/225.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

Alberts, Frederik Nicolaas. "Accurate autonomous landing of a fixed-wing unmanned aerial vehicle." Thesis, Stellenbosch : Stellenbosch University, 2012. http://hdl.handle.net/10019.1/71672.

Full text
Abstract:
Thesis (MScEng)-- Stellenbosch University, 2012.<br>ENGLISH ABSTRACT: This thesis presents the analysis, design, simulation and practical implementation of a control system to achieve an accurate autonomous landing of a fixed-wing unmanned aerial vehicle in the presence of wind gust atmospheric disturbances. Controllers which incorporate the concept of direct-lift control were designed based on a study of the longitudinal dynamics of the UAV constructed as a testbed. Direct-lift control offers the prospect of an improvement in the precision with which aircraft height and vertical velocit
APA, Harvard, Vancouver, ISO, and other styles
4

Phang, Nyit Sin. "Tethered operation of autonomous aerial vehicles to provide extended field of view for autonomous ground vehicles." Thesis, (2 MB), 2006. http://bosun.nps.edu/uhtbin/hyperion.exe/06Dec%5FPhang.pdf.

Full text
Abstract:
Thesis (M.S.)--Naval Postgraduate School, 2006.<br>"December 2006." Includes bibliographical references (p. 47-48). Also available online from the Web site of the Naval Postgraduate School (http://www.nps.edu).
APA, Harvard, Vancouver, ISO, and other styles
5

Sanchez, Sebastian Pablo. "Development and evaluation of a fault detection and identification scheme for the WVU YF-22 UAV using the artificial immune system approach." Morgantown, W. Va. : [West Virginia University Libraries], 2009. http://hdl.handle.net/10450/10399.

Full text
Abstract:
Thesis (M.S.)--West Virginia University, 2009.<br>Title from document title page. Document formatted into pages; contains xiii, 113 p. : ill. (some col.). Includes abstract. Includes bibliographical references (p. 105-110).
APA, Harvard, Vancouver, ISO, and other styles
6

Peddle, Iain K. "Autonomous flight of a model aircraft." Thesis, Stellenbosch : Stellenbosch University, 2005. http://hdl.handle.net/10019.1/2711.

Full text
Abstract:
Thesis (MScEng (Electrical and Electronic Engineering))--Stellenbosch University, 2005.<br>The successful development of a conventional flight autopilot for a model aircraft is presented. All aspects of the autopilot design are considered, from modeling to flight tests. A mathematical aircraft model, as a function of the aircraft’s physical parameters alone, is presented. A controller architecture capable of regulating the motion variables required for conventional flight using only low cost, off-the-shelf sensors is developed. The controller design complements the aircraft model developm
APA, Harvard, Vancouver, ISO, and other styles
7

Meredith, Andre Paul. "An unmanned aircraft system for maritime search and rescue." Thesis, Stellenbosch : University of Stellenbosch, 2011. http://hdl.handle.net/10019.1/6720.

Full text
Abstract:
Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2011.<br>ENGLISH ABSTRACT: Search and Rescue is an essential service provided by States and Militaries to search for, locate and rescue survivors of accidents and incidents. Civil Search and Rescue utilizes a system of well-trained professionals or volunteers, an effective Search and Rescue organization, supported by industry and other providers of infrastructure and assets. The service is rendered to save the lives of civilian individuals in imminent danger of losing their lives. Military (Combat) Search
APA, Harvard, Vancouver, ISO, and other styles
8

De, Hart Ruan Dirk. "Advanced take-off and flight control algorithms for fixed wing unmanned aerial vehicles." Thesis, Stellenbosch : University of Stellenbosch, 2010. http://hdl.handle.net/10019.1/4179.

Full text
Abstract:
Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2010.<br>ENGLISH ABSTRACT: This thesis presents the development and implementation of a position based kinematic guidance system, the derivation and testing of a Dynamic Pursuit Navigation algorithm and a thorough analysis of an aircraft’s runway interactions, which is used to implement automated take-off of a fixed wing UAV. The analysis of the runway is focussed on the aircraft’s lateral modes. Undercarriage and aerodynamic effects are first analysed individually, after which the combined system is anal
APA, Harvard, Vancouver, ISO, and other styles
9

Jagadish, Chirag Chang Bor-Chin. "Fault tolerant attitude sensing and force feedback control for unmanned aerial vehicles /." Philadelphia, Pa. : Drexel University, 2009. http://hdl.handle.net/1860/3071.

Full text
APA, Harvard, Vancouver, ISO, and other styles
10

Quek, Chin Khoon. "Vision based control and target range estimation for small unmanned aerial vehicle." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2005. http://library.nps.navy.mil/uhtbin/hyperion/05Dec%5FQuek.pdf.

Full text
Abstract:
Thesis (M.S. in Engineering Science (Mechanical Engineering))--Naval Postgraduate School, December 2005.<br>Thesis Advisor(s): Isaac I. Kaminer. Includes bibliographical references (p.39). Also available online.
APA, Harvard, Vancouver, ISO, and other styles
More sources

Books on the topic "Drone aircraft. Reliability (Engineering)"

1

Unmanned aviation: A brief history of unmanned aerial vehicles. American Institute of Aeronautics and Astronautics, Inc., 2004.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
2

N, Léchevin, ed. Safety and reliability in cooperating unmanned aerial systems. World Scientific, 2009.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
3

International Symposium on Unmanned Aerial Vehicles (2nd 2009 Reno, Nevada). Selected papers from the 2nd international symposium on UAVs, Reno, Nevada, U.S.A., June 8-10, 2009. Edited by Valavanis K. (Kimon) ed, Beard Randal W. ed, Oh Paul Y. ed, Ollero A. ed, Piegl Les A. ed, and Shim Hyunchui ed. Springer, 2010.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
4

M, Chen Ben, Lee Tong Heng, and SpringerLink (Online service), eds. Unmanned Rotorcraft Systems. Springer-Verlag London Limited, 2011.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
5

Sense and avoid in UAS: Research and applications. Wiley, 2012.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
6

Baker, Robert. Evaluation of reliability modeling tools for advanced fault tolerant systems. Center for Digital Systems Research, Research Triangle Institute, 1986.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
7

United States. Government Accountability Office. Unmanned aircraft systems: DOD needs to more effectively promote interoperability and improve performance assessments : report to the Subcommittee on Tactical Air and Land Forces, Committee on Armed Services, House of Representatives. U.S. Government Accountability Office, 2005.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
8

Krasilʹshchikov, M. N., G. G. Sebri͡akov та K. K. Veremeenko. Sovremennye informat͡sionnye tekhnologii v zadachakh navigat͡sii i navedenii͡a bespilotnykh manevrennykh letatelʹnykh apparatov. Fizmatlit, 2009.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
9

United States. National Transportation Safety Board. Safety report: General aviation crashworthiness project : phase two, impact severity and potential injury prevention in general aviation accidents. The Board, 1985.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
10

United States. National Transportation Safety Board. Safety report: General aviation crashworthiness project : phase III, acceleration loads and velocity changes of survivable general aviation accidents. The Board, 1986.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
More sources

Book chapters on the topic "Drone aircraft. Reliability (Engineering)"

1

Man, Wai Yeung, and Eric T. T. Wong. "Developing Alert Level for Aircraft Components." In Springer Series in Reliability Engineering. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-43412-0_6.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

Anderson, Ronald T., and Lewis Neri. "The Army Aircraft Flight Safety Prediction Model." In Reliability-Centered Maintenance: Management and Engineering Methods. Springer Netherlands, 1990. http://dx.doi.org/10.1007/978-94-009-0757-7_6.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

Chen, Yukun, Lianjun Ou, Gang Rong, and Fei Liu. "Reconfigurable Data Acquisition System with High Reliability for Aircraft." In Lecture Notes in Electrical Engineering. Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-8411-4_54.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

Wang, Xiao-kun, Tie-nan Li, Si-dong Wei, De-xiang Sun, and Li-min Qiao. "Research and Theory Application of Reliability Engineering Management on a Certain Type of Military Transport Aircraft Maintenance Training Simulator." In The 19th International Conference on Industrial Engineering and Engineering Management. Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-38433-2_72.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

"Reliability Assessment of Aircraft Structure Joints under Corrosion-Fatigue Damage." In Engineering Design Reliability Handbook. CRC Press, 2004. http://dx.doi.org/10.1201/9780203483930-33.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

Tuegel, Eric, and Dan Ghiocel. "Reliability Assessment of Aircraft Structure Joints under Corrosion- Fatigue Damage." In Engineering Design Reliability Handbook. CRC Press, 2004. http://dx.doi.org/10.1201/9780203483930.pt3.

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

"Reliability Assessment of Aircraft Structure Joints Under Corrosion-Fatigue Damage." In Engineering Design Reliability Applications. CRC Press, 2007. http://dx.doi.org/10.1201/9781420051339-7.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Tuegel, Eric, and Dan Ghiocel. "Reliability Assessment of Aircraft Structure Joints Under Corrosion-Fatigue Damage." In Engineering Design Reliability Applications. CRC Press, 2007. http://dx.doi.org/10.1201/9781420051339.ch2.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

Verhagen, Wim J. C., and Thijs Oudkerk. "Use of Textual Elements to Improve Reliability Prediction for Aircraft Component Behavior." In Advances in Transdisciplinary Engineering. IOS Press, 2020. http://dx.doi.org/10.3233/atde200116.

Full text
Abstract:
Unplanned maintenance is a costly factor in aircraft operations. Predictive maintenance models aim to provide greater insight into future component and system behaviour. In the state of the art, a variety of statistical models and machine learning techniques, amongst others, are used to estimate component remaining useful life. These approaches commonly leverage technical information, such as sensor data. However, the use of data and techniques from other domains is not prevalent. One such example is the application of natural language processing to incorporate textual information, e.g. derived from pilot complaint data. In other words, does the presence and specific content of pilot complaints have potential to improve the predictability of component removals? In this research, data integration and processing from multiple disciplines are combined to address this question. Relevant words from pilot complaints are identified using a term frequency–inverse document frequency (TF-IDF) numerical analysis, after which the most relevant words are used as covariates in a proportional hazards model. Left truncation and right censoring is applied to limit the time-invariant nature of these covariates. The results in the form of hazard ratios indicate a hazard increase of several orders of magnitude with respect to baseline hazard, pointing towards potential value of including these words as predictive parameters.
APA, Harvard, Vancouver, ISO, and other styles
10

Zenowicz, Kamil, and Wojciech Skarka. "Verification of Flutter Method for the Purposes of Building a Very Flexible Wing Generative Model." In Advances in Transdisciplinary Engineering. IOS Press, 2020. http://dx.doi.org/10.3233/atde200097.

Full text
Abstract:
First step of aircraft design is calculation of initial parameters, based on assumptions determining flight parameters which designed aircraft should meet. During these calculations, it is possible to pre-detect structure instability called a flutter. These calculations are made based on the geometric parameters assumed in the first conceptual drawings of the flying vehicle. Assumed masses and speeds allow for preliminary analysis of forces acting on the structure. The next step is to determine the displacements and deformations occurring in the structure of the aircraft in different phases of flight and under different conditions. The article presents all the stages of wing analysis for a proposed stratospheric drone with a highly flexible wing structure. This analysis, after integration with CAD software, will allow for the preparation of a comprehensive generative model. The basic assumptions of the designed aircraft are: flight altitude, wings area, very extended or unlimited flight time, approximate flight speed, climbing time, hull parameters, rudder size and placement, wing profile and mass of the structure. These assumptions made it possible to carry out a preliminary analysis of loads, wing pressure distribution, lift force and total resistance force. The goal of the research is to develop a methodology of preliminary flutter analysis which can be easily integrated in the form of calculation backgound for generative model. This methodology has been developed to determine displacements, structure stability and critical vibration frequencies. CAD software after integration with constantly optimizing calculation software will allow the generation of optimal shape and structure rigidity for given initial assumptions.
APA, Harvard, Vancouver, ISO, and other styles

Conference papers on the topic "Drone aircraft. Reliability (Engineering)"

1

Reher, Jake, Joan Yule, Eric Fritz, Max Wheeler, Carl A. Nelson, and Larry K. Dungan. "Closed-Loop Control and Release Mechanism Development for Microgravity Free Flyer." In ASME 2014 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/detc2014-35286.

Full text
Abstract:
As human exploration into our solar system expands, the necessity for robotic assistance increases. A free-flying robotic apparatus would be beneficial for space exploration missions to aid humans in small programmed tasks as well as remote planetary or asteroid exploration. The design of these drones would need to account for the fact that much of their time would be spent in a microgravity environment. As this complicates the design, a method for simulating exposure to microgravity was developed by NASA Johnson Space Center: the Active Response Gravity Offload System (ARGOS). ARGOS has been
APA, Harvard, Vancouver, ISO, and other styles
2

Torabbeigi, Maryam, Gino J. Lim, and Seon Jin Kim. "Drone delivery schedule optimization considering the reliability of drones." In 2018 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE, 2018. http://dx.doi.org/10.1109/icuas.2018.8453380.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

Wilson, Richard L. "Ethical issues with use of Drone aircraft." In 2014 IEEE International Symposium on Ethics in Engineering, Science, and Technology (ETHICS). IEEE, 2014. http://dx.doi.org/10.1109/ethics.2014.6893424.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

Fielding, J., and M. Vaziry-Z. "Avionics reliability modelling for aircraft conceptual design." In Aircraft Engineering, Technology, and Operations Congress. American Institute of Aeronautics and Astronautics, 1995. http://dx.doi.org/10.2514/6.1995-3906.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Su, Chang-Qing, and Jia-Jing Jin. "Frequency Reliability Sensitivity Analysis of Aircraft Tension Joints." In 2019 International Conference on Quality, Reliability, Risk, Maintenance, and Safety Engineering (QR2MSE). IEEE, 2019. http://dx.doi.org/10.1109/qr2mse46217.2019.9021136.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

Zhang, Cheng, Xuanping Liao, Fei Guan, and Dongpao Hong. "A synthetic reliability assessment method for aircraft separation systems." In 2015 First International Conference on Reliability Systems Engineering (ICRSE). IEEE, 2015. http://dx.doi.org/10.1109/icrse.2015.7366451.

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

Liu, Chiun-Ming. "Fuzzy-based DEA reliability modeling approach for aircraft engine protection systems." In Industrial Engineering (CIE39). IEEE, 2009. http://dx.doi.org/10.1109/iccie.2009.5223892.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Jiankang, Dong, Ma Hongyan, Chen Jingjie, and Liu Jiaxue. "Mathematical Model of Aircraft Reliability Based on Fault Diagnosis." In 2010 International Conference on Intelligent System Design and Engineering Application (ISDEA). IEEE, 2010. http://dx.doi.org/10.1109/isdea.2010.330.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

Chen, Yuan, Li Du, Yan-Feng Li, Hong-Zhong Huang, and Xiaopeng Li. "FMECA for aircraft electric system." In 2011 International Conference on Quality, Reliability, Risk, Maintenance, and Safety Engineering (ICQR2MSE). IEEE, 2011. http://dx.doi.org/10.1109/icqr2mse.2011.5976581.

Full text
APA, Harvard, Vancouver, ISO, and other styles
10

Wang, Yuanda, Zhe Li, and Jiaao Fu. "Research on effectiveness evaluation of single tanker aircraft." In 2015 First International Conference on Reliability Systems Engineering (ICRSE). IEEE, 2015. http://dx.doi.org/10.1109/icrse.2015.7366424.

Full text
APA, Harvard, Vancouver, ISO, and other styles
You might also be interested in the extended bibliographies on the topic 'Drone aircraft. Reliability (Engineering)' for particular source types:
Journal articles Dissertations / Theses Books
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