Relevant bibliographies by topics / Flight Landing

Contents

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

Academic literature on the topic 'Flight Landing'

Author: Grafiati
Published: 4 June 2021
Last updated: 4 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 'Flight Landing.'

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 "Flight Landing"

1

Jebáček, Ivo, and Marek Horák. "Measuring of a Nose Landing Gear Load during Take-Off and Landing." Applied Mechanics and Materials 821 (January 2016): 325–30. http://dx.doi.org/10.4028/www.scientific.net/amm.821.325.

Full text
Abstract:
This article provides information about in-flight measurement of a small sport aircraft. The strain gauges were used as sensors for load monitoring on the nose landing gear structure. To obtain overall forces it was necessary to do the calibration procedure. After the calculation of strain gauge coefficients the equations for calculating of total force, total force direction and individual force components were determined. During test flights the data acquisition system was installed into the aircraft. The data from strain gauges were collected together with other flight parameters like speed, altitude and data from inertial measurement unit which determined the exact movements of the aircraft before landing. The data recorded during fifty-six flights were analysed to obtain loads acting in the aircraft structure. These results were compared with calculated values.
APA, Harvard, Vancouver, ISO, and other styles
2

Sartor, P., K. Worden, R. K. Schmidt, and D. A. Bond. "Bayesian sensitivity analysis of flight parameters that affect main landing gear yield locations." Aeronautical Journal 118, no. 1210 (December 2014): 1481–97. http://dx.doi.org/10.1017/s0001924000010150.

Full text
Abstract:
Abstract An aircraft and landing gear loads model was developed to assess the Margin of Safety (MS) in main landing gear components such as the main fitting, sliding tube and shock absorber upper diaphragm tube. Using a technique of Bayesian sensitivity analysis, a number of flight parameters were varied in the aircraft and landing gear loads model to gain an understanding of the sensitivity of the MS of the main landing gear components to the individual flight parameters in symmetric two-point landings. The significant flight parameters to the main fitting MS, sliding tube bending moment MS and shock absorber upper diaphragm tube MS include: longitudinal tyre-runway friction coefficient, aircraft vertical descent velocity, aircraft Euler pitch angle and aircraft mass. It was also shown that shock absorber servicing state and tyre pressure do not contribute significantly to the MS.
APA, Harvard, Vancouver, ISO, and other styles
3

Schallhorn, Craig S. "Vigilance Aid Use and Aircraft Carrier Landing Performance in Pilots of Tactical Aircraft." Aerospace Medicine and Human Performance 91, no. 6 (June 1, 2020): 518–24. http://dx.doi.org/10.3357/amhp.5532.2020.

Full text
Abstract:
BACKGROUND: Fatigue is a well-known hazard in aviation. In military fighter communities, policies have evolved to allow for in-flight use of pharmacological vigilance aids to counteract the negative effects of fatigue. With limited objective evidence supporting the role of these medications in continuous flight operations, the present study seeks to evaluate whether use of modafinil is associated with pilot aircraft carrier landing performance.METHODS: A retrospective, observational study was completed following carrier-based flight operations in support of Operation Inherent Resolve. All graded landing passes were included in the analysis. Mixed-effect multivariate linear regression analysis was utilized for the primary outcome of landing signal officer grade of landing performance following combat sorties for events with reported in-flight use of modafinil.RESULTS: A total of 1122 sorties were flown by 79 different pilots with an average landing pass grade of 3.86. The primary outcome of modafinil use in-flight was not generally associated with landing performance. In a subset analysis of more senior ranked aviators, modafinil use appeared to offer a relative performance improvement back to baseline (+0.19). Secondary outcome analysis revealed landing performance was associated with advanced landing technologies (+0.25), sorties later in deployment (+0.05 per 30 d), total career carrier landings (+0.03 per 100 traps), and longer mission duration (-0.04 per hour).DISCUSSION: In the context of evidence supporting subjective benefits of vigilance aid use by aircrew, the results of this study provide ample objective support to the controlled use of modafinil in the operational environment.Schallhorn CS. Vigilance aid use and aircraft carrier landing performance in pilots of tactical aircraft. Aerosp Med Hum Perform. 2020; 91(6):518–524.
APA, Harvard, Vancouver, ISO, and other styles
4

Feng, Xiao Rong, Xing Jie Feng, and Dong Liu. "The Application of Ant Colony Optimization Algorithm in the Flight Landing Scheduling Problem." Applied Mechanics and Materials 411-414 (September 2013): 2698–703. http://dx.doi.org/10.4028/www.scientific.net/amm.411-414.2698.

Full text
Abstract:
Flights landing scheduling problem is an NP-hard problem, the article presents an Ant colony optimization algorithm based on dynamic calculation of the heuristic information to solve a single runway flights landing scheduling problem. The algorithm has better global search ability and relatively fast convergence rate. The experimental results show that compared with traditional first come first serve, genetic algorithm and particle swarm algorithm, this method can quickly give the better flight approach and landing order to help controllers make efficient aircraft scheduling policy and reduce flight delays. Keywords:Heuristic Information entropy Ant colony optimization Global search
APA, Harvard, Vancouver, ISO, and other styles
5

Muijres, Florian T., Coby van Dooremalen, Martin Lankheet, Heleen Lugt, Lana J. de Vries, and Frank Van Langevelde. "Varroa destructor infestation impairs the improvement of landing performance in foraging honeybees." Royal Society Open Science 7, no. 9 (September 2020): 201222. http://dx.doi.org/10.1098/rsos.201222.

Full text
Abstract:
The parasitic mite Varroa destructor is an important contributor to the high losses of western honeybees. Forager bees from Varroa -infested colonies show reduced homing and flight capacity; it is not known whether flight manoeuvrability and related learning capability are also affected. Here, we test how honeybees from Varroa -infested and control colonies fly in an environment that is unfamiliar at the beginning of each experimental day. Using stereoscopic high-speed videography, we analysed 555 landing manoeuvres recorded during 12 days of approximately 5 h in length. From this, we quantified landing success as percentage of successful landings, and assessed how this changed over time. We found that the forager workforce of Varroa -infested colonies did not improve their landing success over time, while for control bees landing success improved with approximately 10% each hour. Analysis of the landing trajectories showed that control bees improved landing success by increasing the ratio between in-flight aerodynamic braking and braking at impact on the landing platform; bees from Varroa -infested colonies did not increase this ratio over time. The Varroa -induced detriment to this landing skill-learning capability might limit forager bees from Varroa -infested colonies to adapt to new or challenging conditions; this might consequently contribute to Varroa -induced mortality of honeybee colonies.
APA, Harvard, Vancouver, ISO, and other styles
6

Green, P. R., and P. Cheng. "Variation in kinematics and dynamics of the landing flights of pigeons on a novel perch." Journal of Experimental Biology 201, no. 24 (December 15, 1998): 3309–16. http://dx.doi.org/10.1242/jeb.201.24.3309.

Full text
Abstract:
Pigeons made 10 flights to a novel perch. Kinematic measurements of these flights were obtained from video recordings, and the forces exerted on the perch on each landing were measured. There was wide variation(20-fold range) in the kinetic energy of the pigeons just before landing,arising almost entirely from variation in horizontal velocity. The maximum force exerted on the perch varied in magnitude from approximately twice to eight times the pigeons' body weight, and in direction from 40 to 90 below the horizontal. In landings with high final kinetic energy, the maximum force exerted on the perch was larger and was applied at a shallower angle than in those with low final kinetic energy. Landing flights with high final kinetic energy showed straighter trajectories and a larger peak deceleration during the last 300 ms of approach flight than those with low final kinetic energy, which had downward-curving trajectories and a more prolonged and steady pattern of deceleration. Mean final kinetic energy was lower in the first two landings made on the perch than in subsequent landings, indicating that pigeons are more likely to adopt a slow,downward-curving approach to a novel perch and a fast, straight approach to a familiar one.
APA, Harvard, Vancouver, ISO, and other styles
7

Afanas’ev, V. A., G. L. Degtyarev, A. S. Meshchanov, and R. T. Sirazetdinov. "Landing of flight vehicles without the landing gear." Russian Aeronautics (Iz VUZ) 57, no. 4 (October 2014): 339–43. http://dx.doi.org/10.3103/s1068799814040035.

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

Motoda, Toshikazu, Yoshikazu Miyazawa, Kazutoshi Ishikawa, and Tatsushi Izumi. "Automatic landing flight experiment flight simulation analysis and flight testing." Journal of Spacecraft and Rockets 36, no. 4 (July 1999): 554–60. http://dx.doi.org/10.2514/3.27199.

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

Öznalbant, Zafer, and Mehmet Ş. Kavsaoğlu. "Flight control and flight experiments of a tilt-propeller VTOL UAV." Transactions of the Institute of Measurement and Control 40, no. 8 (February 26, 2018): 2454–65. http://dx.doi.org/10.1177/0142331218754618.

Full text
Abstract:
The purpose of this work is to present a study on the stability and control of an unmanned, fixed wing, vertical take-off and landing aerial vehicle. This airplane is driven by a fixed-pitch tilt-propeller system with the capability of vertical take-off and landing as well as conventional flight. The novelty of the vehicle is the use of a fixed-pitch propeller system instead of variable-pitch tilt-rotors. There are three flight modes: vertical, transitional and conventional flight modes. Each flight mode has different dynamic characteristics. Therefore, these modes each need dedicated flight control methods. In this paper, the equations of motion are generated by modelling the aerodynamic and propulsion forces and moments. After performing trim condition calculations, longitudinal stability characteristics are investigated for each flight mode. The control methods are described for vertical, transitional and conventional flight modes. Stability augmentation systems, which consist of proportional and proportional/integral controller, are applied. A number of flight tests, including vertical, transitional and conventional flights, have been successfully performed with a prototype aircraft.
APA, Harvard, Vancouver, ISO, and other styles
10

Gregory, Kevin B., Rhiannon N. Soriano-Smith, Amanda C. M. Lamp, Cassie J. Hilditch, Michael J. Rempe, Erin E. Flynn-Evans, and Gregory L. Belenky. "Flight Crew Alertness and Sleep Relative to Timing of In-Flight Rest Periods in Long-Haul Flights." Aerospace Medicine and Human Performance 92, no. 2 (February 1, 2021): 83–91. http://dx.doi.org/10.3357/amhp.5672.2021.

Full text
Abstract:
BACKGROUND: In-flight breaks are used during augmented long-haul flight operations, allowing pilots a sleep opportunity. The U.S. Federal Aviation Administration duty and rest regulations restrict the pilot flying the landing to using the third rest break. It is unclear how effective these restrictions are on pilots ability to obtain sleep. We hypothesized there would be no difference in self-reported sleep, alertness, and fatigue between pilots taking the second vs. third rest breaks.METHODS: Pilots flying augmented operations in two U.S.-based commercial airlines were eligible for the study. Volunteers completed a survey at top-of-descent (TOD), including self-reported in-flight sleep duration, and Samn-Perelli fatigue and Karolinska Sleepiness Scale ratings. We compared the second to third rest break using noninferiority analysis. The influence of time of day (home-base time; HBT) was evaluated in 4-h blocks using repeated measures ANOVA.RESULTS: From 787 flights 500 pilots provided complete data. The second rest break was noninferior to the third break for self-reported sleep duration (1.5 0.7 h vs. 1.4 0.7 h), fatigue (2.0 1.0 vs. 2.9 1.3), and sleepiness (2.6 1.4 vs. 3.8 1.8) at TOD for landing pilots. Measures of sleep duration, fatigue, and sleepiness were influenced by HBT circadian time of day.DISCUSSION: We conclude that self-reported in-flight sleep, fatigue, and sleepiness from landing pilots taking the second in-flight rest break are equivalent to or better than pilots taking the third break. Our findings support providing pilots with choice in taking the second or third in-flight rest break during augmented operations.Gregory KB, Soriano-Smith RN, Lamp ACM, Hilditch CJ, Rempe MJ, Flynn-Evans EE, Belenky GL. Flight crew alertness and sleep relative to timing of in-flight rest periods in long-haul flights. Aerosp Med Hum Perform. 2021; 92(2):8391.
APA, Harvard, Vancouver, ISO, and other styles
More sources

Dissertations / Theses on the topic "Flight Landing"

1

Hooper, Jack Charles. "Vertical landing flight envelope definition." Thesis, Luleå tekniska universitet, Rymdteknik, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-80717.

Full text
Abstract:
This paper will investigate the development of a landing footprint for a re-entry vehicle. Vehicles can re-enter the atmosphere with a range of orientations, velocities and flight path angles. The central question is whether a vehicle with any combination of these states can be brought to an acceptable landing condition at a particular landing site and with a particular landing speed. To aide in this investigation several models must be implemented, including that of the atmosphere, the vehicles, the Earth, and the aerodynamics. A detailed analysis of the aerodynamic model will be treated, and the equations of motion subject to these aerodynamic laws will then be compared to results from existing atmospheric reentry software. The principles of optimization will then be employed to generate the footprint of landable states, based on maximum and minimum possible downrange distances, for two vehicle concepts.
APA, Harvard, Vancouver, ISO, and other styles
2

Fitzgerald, Pio. "Flight control system design for autonomous UAV carrier landing." Thesis, Cranfield University, 2004. http://hdl.handle.net/1826/840.

Full text
Abstract:
The challenge of integrating the UAV fleet into the carrier landing operational structure with respect to navigation and control strategies is addressed. A simulation model was developed which includes an aircraft model, an atmosphere model and an aircraft carrier motion model. The six degree of freedom non-linear aircraft model is based on the aerodynamic characteristics of the Mk 4a Jindivik extended to include rudder, spoiler and thrust vectoring controls, and an undercarriage model. The atmosphere model includes a carrier landing atmospheric disturbance model. The six degree of freedom aircraft carrier motion model is based on the ship motion simulation program SEAWAY. A Navigation System was developed which conforms to current operational procedures and future military navigation goals. This Navigation System continuously predicts the position in space where touchdown on the carrier deck will take place, based on aircraft position, the relative velocity between the aircraft and carrier, and the motion time history of the carrier. A reference flight path to the predicted touchdown point is continuously defined. The aircraft deviation from this flight path is determined and input to the autoland control system. For the purposes of this study perfection prediction is assumed. Automatic flight control systems were developed to assess three control strategies for suitability to the carrier landing task. The focus of this assessment was on vertical glide path deviation control. Direct Lift Control was compared to conventional control and was found to have superior performance, especially in turbulence. As UAV planforms tend to be tailless, and therefore lateral and pitch control are generated by a common aerodynamic surface, thrust vectoring was investigated as a means of alleviating aerodynamic pitch control requirements in the carrier landing task. An Adaptive Approach Speed Controller was developed as an extension of the Navigation System. This system synchronises the time that the aircraft passes over the stern, or ramp, of the carrier with the minimum absolute carrier pitch attitude attainable for a given range of approach speeds. This system was shown to be an effective method of minimising the negative effect that carrier motion has on the clearance between the aircraft and the carrier’s ramp.
APA, Harvard, Vancouver, ISO, and other styles
3

Wakefield, Nigel Hugh. "Helicopter flight in the airwake of non-aviation ships." Thesis, University of Southampton, 2000. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.326729.

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

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.

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

Roback, Vincent Eric. "Characterization and Helicopter Flight Test of 3-D Imaging Flash LIDAR Technology for Safe, Autonomous, and Precise Planetary Landing." Thesis, Virginia Tech, 2012. http://hdl.handle.net/10919/76845.

Full text
Abstract:
Two flash lidars, integrated from a number of cutting-edge components from industry and NASA, are lab characterized and flight tested under the Autonomous Landing and Hazard Avoidance (ALHAT) project (in its fourth development and field test cycle) which is seeking to develop a guidance, navigation, and control (GNC) and sensing system based on lidar technology capable of enabling safe, precise human-crewed or robotic landings in challenging terrain on planetary bodies under any ambient lighting conditions. The flash lidars incorporate pioneering 3-D imaging cameras based on Indium-Gallium-Arsenide Avalanche Photo Diode (InGaAs APD) and novel micro-electronic technology for a 128 x 128 pixel array operating at 30 Hz, high pulse-energy 1.06 ?m Nd:YAG lasers, and high performance transmitter and receiver fixed and zoom optics. The two flash lidars are characterized on the NASA-Langley Research Center (LaRC) Sensor Test Range, integrated with other portions of the ALHAT GNC system from around the country into an instrument pod at NASA-JPL, integrated onto an Erickson Aircrane Helicopter at NASA-Dryden, and flight tested at the Edwards AFB Rogers dry lakebed over a field of human-made geometric hazards. Results show that the maximum operational range goal of 1000m is met and exceeded up to a value of 1200m, that the range precision goal of 8 cm is marginally met, and that the transmitter zoom optics divergence needs to be extended another eight degrees to meet the zoom goal 6° to 24°. Several hazards are imaged at medium ranges to provide three-dimensional Digital Elevation Map (DEM) information.
Master of Science
APA, Harvard, Vancouver, ISO, and other styles
6

Visser, Bernardus Johannes. "Presisie landing van 'n onbemande vliegtuig." Thesis, Stellenbosch : Stellenbosch University, 2008. http://hdl.handle.net/10019.1/2160.

Full text
Abstract:
Thesis (MScEng (Electrical and Electronic Engineering)--Stellenbosch University, 2008.
This thesis presents the design of a control system for the autonomous precision landing of an unmanned aerial vehicle aided by an infra red camera for precision position measurements. An optimal kinematics state estimator was designed using two Kalman filters. A Monocular vision algorithm that uses markers on the runway was developed to supply accurate position measurements on the final approach of the landing. Inner-loop controllers as proposed by [14] and implemented in [5] are used to reduce the aircraft dynamics to a point mass with steerable acceleration vector. Outer-loop controllers as proposed by [13] were modified and expanded to guide the aircraft on the circuit and final approach. The hardware in the loop simulator that was designed in [6] was expanded for optical measurements and used to verify the system. An infra red camera node was designed and built to supply the optical measurements. The system was installed on a model aircraft and partially tested with practical test flights.
APA, Harvard, Vancouver, ISO, and other styles
7

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.

Full text
Abstract:
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 pilots were flying over Populated area at Final Approach to L/D phase, they showed lower performance on tracking the glide path. Based on the results, stresses and workload can have a significant impact on flight performance. Therefore, in order to reduce the workload and stress that can cause human errors, it is highly recommended to carefully examine the impact of new flight procedures on pilot workload and stress before they are implemented.; Since human errors are one of the major causes of flight accidents, the design and operation of the modern aircraft system deals with them seriously. Particularly, the pilot workload on aviation causes human errors. Whenever new procedures are introduced and operated, the aircraft capabilities have been checked in every aspect. However, there has been little study on the impact of the new procedures such as LDLP, SCDA, SATS, and Steep Angle approach on the pilot performance, workload, and stress. In this study, different methods have been tried to understand the relationship between new procedures and the pilots in terms of performance, workload, and stress. The flight factors (e.g. flight experience, gliding angle, and approach area) were examined by the pilot performance, workload, and stress at the "Final Approach to L/D" phase using the single engine Cessna 172R type flight simulator. Five students and five instructor pilots from Embry-Riddle Aeronautical University in Dayton Beach, Florida, participated and they flew under four different simulation tasks of gliding angle and approach area. Their Heart Rate Variability (HRV) and NASA-Task Load Index (TLX) were measured to determine their stress level and subjective workload, respectively. In addition, Landing Performance (LP) data (e.g. landing distance, landing speed) and Above Glide Path Tracking Performance (AGPTP) data were also collected to evaluate pilot performance. As a result, the type of approach area showed a significant effect on pilot performance, workload, and stress determined by ANOVA (HRV, TLX, LP, AGPTP: all are p less than] .05). Flying over "Populated" area (e.g. a large city) resulted in lower pilot performance and higher pilot workload and stress than that over "Non-Populated" area (e.g. a grass field).
ID: 029049593; System requirements: World Wide Web browser and PDF reader.; Mode of access: World Wide Web.; Thesis (Ph.D.)--University of Central Florida, 2010.; Includes bibliographical references (p. 95-112).
Ph.D.
Doctorate
Department of Industrial Engineering and Management Systems
Engineering and Computer Science
APA, Harvard, Vancouver, ISO, and other styles
8

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.

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

Grymin, David J. "Development of a novel method for autonomous navigation and landing of unmanned aerial vehicles /." Online version of thesis, 2009. http://hdl.handle.net/1850/10615.

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

Murphy, Timothy A. "MLS Flight inspection techniques: Digital filtering and coordinate transformation." Ohio : Ohio University, 1985. http://www.ohiolink.edu/etd/view.cgi?ohiou1184070645.

Full text
APA, Harvard, Vancouver, ISO, and other styles
More sources

Books on the topic "Flight Landing"

1

First landing. New York: Ace Books, 2001.

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

Transportation Safety Board of Canada. Flight in unfavourable weather, Flight 80, Canuck C-FEBF, Holden Lake, Quebec, 14 March 1994. Hull, Quebec: Transportation Safety Board of Canada, 1994.

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

Higgins, Nadia. Moon landing. Edina, Minn: ABDO Pub. Co., 2008.

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

Hueschen, Richard M. Implementation and flight tests for the digital integrated automatic landing system (DIALS). Hampton, Va: National Aeronautics and Space Administration ,Langley Research Center, 1986.

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

Donoghue, Emma. Landing. Orlando: Harcourt, 2007.

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

Transportation Safety Board of Canada. VFR flight into IMC - loss of control, Southern Interior Flight Centre Ltd., Cessna 172M C-GIWX, Hope Slide, British Columbia, 24 April 1994. Hull, Quebec: Transportation Safety Board of Canada, 1994.

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

Canada, Transportation Safety Board of. Controlled flight into terrain, Preferred Flights Inc., Piper PA31-350 Navajo Chieftain C-GNPG, Bathurst, New Brunswick, 04 January 1994. Hull, Quebec: Transportation Safety Board of Canada, 1994.

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

Dunn, Joeming W. Moon landing. Edina, Minn: Red Wagon, 2008.

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

Erkelens, L. J. J. Flight simulator evaluation of advanced MLS procedures. Amsterdam: National Aerospace Laboratory, 1991.

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

FEDERAL AVIATION ADMINISTRATION. Flight Management System (FMS) instrument procedures development. [Washington, D.C.?]: U.S. Dept. of Transportation, Federal Aviation Administration, 1996.

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

Book chapters on the topic "Flight Landing"

1

Abdallah, Lina. "Optimal Flight Paths Reducing the Aircraft Noise during Landing." In Communications in Computer and Information Science, 1–10. Berlin, Heidelberg: Springer Berlin Heidelberg, 2008. http://dx.doi.org/10.1007/978-3-540-87477-5_1.

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

Baburov S.V., Bestugin A.R., Galyamov A.M., Sauta O.I., and Shatrakov Y.G. "Methodology for Constructing Satellite-Based Landing Systems and Collision Avoidance Systems." In Development of Navigation Technology for Flight Safety, 43–77. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-8375-5_2.

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

Baburov S.V., Bestugin A.R., Galyamov A.M., Sauta O.I., and Shatrakov Y.G. "Methods for Improving Flight Efficiency and Safety for Satellite-Based Landing Systems." In Development of Navigation Technology for Flight Safety, 79–120. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-8375-5_3.

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

Wang, Lei, Yong Ren, Hui Sun, and Chuanting Dong. "A Landing Operation Performance Evaluation System Based on Flight Data." In Engineering Psychology and Cognitive Ergonomics: Cognition and Design, 297–305. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-58475-1_22.

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

Hu, C., S. Zhou, Y. Xie, and W. Chang. "The Markov forecasting model of landing states based on flight data." In Risk, Reliability and Safety: Innovating Theory and Practice, 2277–81. Taylor & Francis Group, 6000 Broken Sound Parkway NW, Suite 300, Boca Raton, FL 33487-2742: CRC Press, 2016. http://dx.doi.org/10.1201/9781315374987-343.

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

Wang, Lei, Changxu Wu, Ruishan Sun, and Zhenxin Cui. "An Analysis of Hard Landing Incidents Based on Flight QAR Data." In Engineering Psychology and Cognitive Ergonomics, 398–406. Cham: Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-07515-0_40.

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

Nonami, Kenzo, Farid Kendoul, Satoshi Suzuki, Wei Wang, and Daisuke Nakazawa. "Autonomous Indoor Flight and Precise Automated-Landing Using Infrared and Ultrasonic Sensors." In Autonomous Flying Robots, 303–22. Tokyo: Springer Japan, 2010. http://dx.doi.org/10.1007/978-4-431-53856-1_13.

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

Wang, Lei, Changxu Wu, and Ruishan Sun. "Pilot Operating Characteristics Analysis of Long Landing Based on Flight QAR Data." In Lecture Notes in Computer Science, 157–66. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-39354-9_18.

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

Baburov S.V., Bestugin A.R., Galyamov A.M., Sauta O.I., and Shatrakov Y.G. "Integrated Technical Solutions on the Joint Use of Technologies Applicable in Collision Avoidance Systems and Satellite-Based Landing Systems." In Development of Navigation Technology for Flight Safety, 161–98. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-8375-5_5.

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

Baburov S.V., Bestugin A.R., Galyamov A.M., Sauta O.I., and Shatrakov Y.G. "Recommendations for the Application of the Proposed Technical Solutions in the Satellite-Based Landing Systems and Collision Avoidance Systems." In Development of Navigation Technology for Flight Safety, 199–228. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-8375-5_6.

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

Conference papers on the topic "Flight Landing"

1

Manivannan, Vasudevan, Jared P. Langley, Mark Costello, and Massimo Ruzzene. "Rotorcraft Slope Landings with Articulated Landing Gear." In AIAA Atmospheric Flight Mechanics (AFM) Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-5160.

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

Abzug, Malcolm. "An unconventional tricycle landing gear." In 24th Atmospheric Flight Mechanics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-4018.

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

Peer, David B. "Flight Deck Landing Load Diagrams." In Warship 2000: Warships for Amphibious Operations & Minewarfare. RINA, 2000. http://dx.doi.org/10.3940/rina.ws.2000.07.

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

DIDOMENICO, E., and D. BIEZAD. "Loop Separation Parameter for landing flying qualities." In 12th Atmospheric Flight Mechanics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1985. http://dx.doi.org/10.2514/6.1985-1788.

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

Nuthi, Pavan Kumar, and Kamesh Subbarao. "Autonomous vertical landing on a marine vessel." In AIAA Atmospheric Flight Mechanics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2014. http://dx.doi.org/10.2514/6.2014-0034.

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

LEE, A., A. BRYSON, JR., and W. HINDSON. "Optimal landing of a helicopter in autorotation." In 13th Atmospheric Flight Mechanics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-2287.

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

Carvalho, Bruno J. "Airborne Landing Distance: A Neural Network Approach." In AIAA Atmospheric Flight Mechanics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2016. http://dx.doi.org/10.2514/6.2016-3103.

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

Miyazawa, Yoshikazu, Kazutoshi Ishikawa, Toshikazu Motoda, Tatsushi Izumi, Masakazu Sagisaka, Takashi Hata, and Hiroyuki Onuma. "Flight control system for the Automatic Landing Flight Experiment." In Guidance, Navigation, and Control Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1996. http://dx.doi.org/10.2514/6.1996-3782.

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

Novak, A., and J. Pitor. "Flight inspection of instrument landing system." In 2011 IEEE Forum on Integrated and Sustainable Transportation Systems (FISTS 2011). IEEE, 2011. http://dx.doi.org/10.1109/fists.2011.5973617.

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

MCCUSKER, TODD, and STEVEN HILL. "Landing dispersions for the Commercial Experiment Transporter Recovery System." In Flight Simulation and Technologies. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-3695.

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

Reports on the topic "Flight Landing"

1

NAVAL AIR SYSTEMS COMMAND PATUXENT RIVER MD. Procedures For Submitting Flight Loads, Launch, and Landing Data for the Structural Appraisal of Fatigue Effects Program. Fort Belvoir, VA: Defense Technical Information Center, November 2000. http://dx.doi.org/10.21236/ada384646.

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

NAVAL AIR SYSTEMS COMMAND PATUXENT RIVER MD. Procedures for Submitting Flight Loads, Launch, and Landing Data for the Structural Appraisal of Fatigue Effects Program. Fort Belvoir, VA: Defense Technical Information Center, February 1999. http://dx.doi.org/10.21236/ada384654.

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

Newman, Richard L., and Randall E. Bailey. Improvement of Head-Up Display Standards. Volume 5. Head Up Display ILS (Instrument Landing System) Accuracy Flight Tests. Fort Belvoir, VA: Defense Technical Information Center, September 1987. http://dx.doi.org/10.21236/ada194602.

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

Picard, Mary. F/A-18A/B/C/D Main Landing Gear Control Unit Hydraulic 2A Supply Line Pressure Spikes and Emergency Port Restrictor Ground and Flight Tests Evaluation. Fort Belvoir, VA: Defense Technical Information Center, November 2002. http://dx.doi.org/10.21236/ada409130.

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

Doo, Johnny. Unsettled Issues Concerning the Opportunities and Challenges of eVTOL Applications during a Global Pandemic. SAE International, October 2020. http://dx.doi.org/10.4271/epr2020022.

Full text
Abstract:
Electric vertical takeoff and landing (eVTOL) aircraft technology has developed beyond the traditional aviation industry and now influences the creation of new and novel transportation applications. Some experts even suggest on-demand eVTOL logistics capabilities could be harnessed by crisis response teams to c ombat a future pandemic. The lessons of the COVID-19 crisis highlighted the challenges of managing a global pandemic response due to the difference in regional and local resources, culture, and political systems. Although there may not be a uniform crisis management strategy that the world can agree on, next-generation vertical flight vehicles could be used to distribute limited medical equipment, supplies, and personnel to hot spots faster than conventional aircraft or ground vehicles. However, creating this capability is not easy. This SAE EDGE™ Research Report by Johnny Doo addresses the opportunities and challenges of establishing an eVTOL fleet, including deployment, supporting infrastructure, and fleet management.
APA, Harvard, Vancouver, ISO, and other styles
6

Wagner, Mike, and Chuck Webb. VMCA Flight Test of the Carrier-Landin', Mail-Hauling' C-2A. Fort Belvoir, VA: Defense Technical Information Center, April 2000. http://dx.doi.org/10.21236/ada377905.

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

Anderton, Gary, Ernest Berney, John Newman, Travis Mann, Chad Gartrell, and Daniel Miller. Joint Rapid Airfield Construction (JRAC) Program 2004 Demonstration Project--Fort Bragg, North Carolina. Engineer Research and Development Center (U.S.), March 2021. http://dx.doi.org/10.21079/11681/40139.

Full text
Abstract:
This report describes the demonstration of technologies and procedures developed during April 2002 and May 2004 under the Joint Rapid Airfield Construction (JRAC) Program. The demonstration took place at Sicily Landing Zone (LZ) at Fort Bragg, NC, in July of 2004. The objective of the exercise was to demonstrate the procedures and technologies developed under the JRAC Program by rapidly building two parking aprons capable of supporting C-130 transport aircraft taxiing and parking operations. The exercise was conducted under continuous 24-hr operations to simulate a real-world rapid construction environment. Apron 1 (north apron) was constructed using two technologies, one-half being ACE™ Matting and the other half being a cement-polymer stabilized soil surface. Apron 2 (south apron) was constructed solely of a fiber-cement-stabilized soil system. Both aprons were treated with a polymer emulsion surface application to form a sealed surface against abrasion and water infiltration. The entire construction of both aprons required 76 hr, with Apron 1 finished in 48 hr. The construction of Apron 1 was validated by operation of a C-130 aircraft approximately 31 hr after completion with success and high praises from the aircraft flight crew on the stability and surface of the apron, as well as its dust-abating characteristics.
APA, Harvard, Vancouver, ISO, and other styles
You might also be interested in the extended bibliographies on the topic 'Flight Landing' 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