Relevant bibliographies by topics / Flights control center

Contents

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

Academic literature on the topic 'Flights control center'

Author: Grafiati
Published: 30 May 2022
Last updated: 31 July 2025

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Journal articles on the topic "Flights control center"

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Khabibullin, R. M., and O. L. Starinova. "Non-coplanar interplanetary flight simulation considering motion relative to the center of mass peculiarities of solar sail spacecraft." Spacecrafts & Technologies 4, no. 3 (2020): 141–50. http://dx.doi.org/10.26732/j.st.2020.3.02.

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The paper is devoted to the non-coplanar interplanetary Earth–Venus flight of a spacecraft equipped with a non-perfectly reflecting solar sail, the magnitude and direction of acceleration from which is calculated taking into account specular and diffuse reflections, absorption and transmission of photons by the surface of the solar sail. The goal of the heliocentric motion is to transfer the solar sail spacecraft into the Hill sphere of Venus with zero hyperbolic excess of speed. A feature of the paper is the study of the motion of a non-perfectly reflecting solar sail spacecraft taking into a
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Fruncillo, Felice, Luigi Federico, Marco Cicala, and Roberto Citarella. "Development and Validation of an Aeropropulsive and Aeroacoustic Simulation Model of a Quadcopter Drone." Drones 6, no. 6 (2022): 143. http://dx.doi.org/10.3390/drones6060143.

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In the present work a dynamic simulation model for a quadcopter drone is developed and validated through experimental flight data. The aerodynamics of the rotors is modeled with the blade element theory combined with the Peters and He dynamic wake model, using an appropriate number of states. The aerodynamic forces and moments thus calculated feed the dynamic equations of a drone and an aeroacoustics model, to obtain an estimate of the noise generated during the flight. Loading and thickness noise are calculated as a time domain solution of the wave equation (Farassat 1A formulation), with mob
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Roshanbin, A., H. Altartouri, M. Karásek, and A. Preumont. "COLIBRI: A hovering flapping twin-wing robot." International Journal of Micro Air Vehicles 9, no. 4 (2017): 270–82. http://dx.doi.org/10.1177/1756829317695563.

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This paper describes the results of a six-year project aiming at designing and constructing a flapping twin-wing robot of the size of hummingbird ( Colibri in French) capable of hovering. Our prototype has a total mass of 22 g, a wing span of 21 cm and a flapping frequency of 22 Hz; it is actively stabilized in pitch and roll by changing the wing camber with a mechanism known as wing twist modulation. The proposed design of wing twist modulation effectively alters the mean lift vector with respect to the center of gravity by reorganization of the airflow. This mechanism is modulated by an onbo
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Muliasari, Ataline. "Upaya Bandara Ngurah Rai Denpasar Dalam Mewujudkan Safety Management System (SMS)." Warta Penelitian Perhubungan 22, no. 5 (2010): 481–96. http://dx.doi.org/10.25104/warlit.v22i5.1113.

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Each airport management including Denpasar Ngurah Rai International Airport are required tocreate, implement, eunluate and impmue the sustainnble safe~; rruznagement si;stem (SMS) with asafehJ program based on intemntionnl mzd nntionnl flight s. Relnted to the nhaue, ns nn internationalairport located in the center of touris111 lcxatio11 of hzdonesin, Nguralt Rni lntenuztional Airport tnjingto realize its SafehJ Management System (SMS). Ihis condition is certainly important to be realizedconsidering the level of aircraft mauements for both international and national flights is very high atthis
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Soldatenko, A. V., V. F. Pivovarov, O. N. Pyshnaya, L. K. Gurkina, and M. M. Tareeva. "Greenhouses in space: from intention to implementation." Vegetable crops of Russia, no. 2 (April 6, 2023): 5–10. http://dx.doi.org/10.18619/2072-9146-2023-2-5-10.

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April 12 is Cosmonautics Day, International Day of Human Space Flight. This is a memorable date dedicated to the flight of the first cosmonaut of the planet, Yuri Alekseevich Gagarin, who became a symbol of the earthlings' dream come true. The All-Russian Research Institute of Vegetable Breeding and Seed Production (Federal State Budgetary Scientific Institution Federal Scientific Vegetable Center (FSBSI FSVC)), like a number of other academic institutions, from the beginning of space exploration, got involved in the work to solve the problem of developing food for astronauts and continues res
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Hoang Quan, Nguyen Ngoc, and V. N. Nechaev. "Proposals for designing the airspace management of the ATM sectors of the Ho Chi Minh City Area Control Center to increase its capacity." Civil Aviation High Technologies 27, no. 3 (2024): 50–66. http://dx.doi.org/10.26467/2079-0619-2024-27-3-50-66.

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According to the International Air Transport Association (IATA), Vietnam is among the countries with the rapid development of civil aviation (CA). This development is a positive sign to enhance the role and position of Vietnam civil aviation in the civil aviation community. But at the same time, the increase in flight operations poses challenges to flight safety, increases the load on airspace and airports, and pollutes the environment. The Ho Chi Minh City (HCM) airspace is one of the largest and busiest airspace in Southeast Asia. Every year, thousands of flights depart, arrive, and cross th
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Atallah, Stephanie, and Susan Hotle. "Evaluation of Airport Size and Delay Causal Factor Effects on Delay Propagation Dissipation." Transportation Research Record: Journal of the Transportation Research Board 2676, no. 3 (2021): 608–20. http://dx.doi.org/10.1177/03611981211055663.

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The International Civil Aviation Organization identifies departure and arrival punctuality as on-time key performance indicators. However, these metrics assume a flight’s delay is a result of either the origin or destination airport, providing limited information on where delay should be mitigated in the U.S. National Airspace System (NAS). This study evaluates the relationship between delay propagation magnitude, delay causal factor, airport size, and charged facility (airport or Air Route Traffic Control Center), to examine if certain delays take longer to dissipate. First, using flights fro
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Huang, Lixiao, Victoria Chibuogu Nneji, and Mary Cummings. "How Airline Dispatchers Manage Flights: A Task Analysis in Distributed and Heterogeneous Network Operations." Proceedings of the Human Factors and Ergonomics Society Annual Meeting 63, no. 1 (2019): 1389–93. http://dx.doi.org/10.1177/1071181319631182.

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Equipped with technology, airline dispatchers interact with multiple entities to maximize the safety and efficiency of flights. How well the overall airline system performs is influenced by dispatchers’ workload. In order to assist future work in developing advanced automated technologies to assist dispatchers, particularly under high-workload periods, this paper presents an analysis of airline dispatchers’ tasks in a large operations control center. This is an important step in developing airline dispatcher workload simulations and other analytical approaches that assist in staffing of operat
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Speese, John. "Soil and Foliar Insecticides to Control Insects in Sweet Potatoes, Painter, VA, 1994." Arthropod Management Tests 20, no. 1 (1995): 133. http://dx.doi.org/10.1093/amt/20.1.133a.

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Abstract Sweet potatoes were planted on 17 Jun at the Eastern Shore Agricultural Research and Extension Center, Painter, VA. Each plot consisted of 3 rows 20 ft long on 3 ft spacing, replicated six times in a randomized, complete block design. A single untreated guard row separated each plot. Soil treatments were applied immediately prior to planting in the manner indicated in the table and incorporated. Lorsban 4E and Fipronil 80WG were applied using a 6 flat fan nozzle boom backpack sprayer delivering 20 gal water/acre at 40 psi. The gallonage was increased to 40 gal/acre for the Sevin folia
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Fu, Yu, Shaofu Lin, and Zhenkai Xu. "Research on Quantitative Analysis of Multiple Factors Affecting COVID-19 Spread." International Journal of Environmental Research and Public Health 19, no. 6 (2022): 3187. http://dx.doi.org/10.3390/ijerph19063187.

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The Corona Virus Disease 2019 (COVID-19) is spreading all over the world. Quantitative analysis of the effects of various factors on the spread of the epidemic will help people better understand the transmission characteristics of SARS-CoV-2, thus providing a theoretical basis for governments to develop epidemic prevention and control strategies. This article uses public data sets from The Center for Systems Science and Engineering at Johns Hopkins University (JHU CSSE), Air Quality Open Data Platform, China Meteorological Data Network, and WorldPop website to construct experimental data. The
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Dissertations / Theses on the topic "Flights control center"

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Williams, Steve. "Advanced Test Range Verification at RF Without Flights." International Foundation for Telemetering, 2010. http://hdl.handle.net/10150/605960.

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ITC/USA 2010 Conference Proceedings / The Forty-Sixth Annual International Telemetering Conference and Technical Exhibition / October 25-28, 2010 / Town and Country Resort & Convention Center, San Diego, California<br>Flight and weapons test ranges typically include multiple Telemetry Sites (TM Sites) that receive telemetry from platforms being flown on the range. Received telemetry is processed and forwarded by them to a Range Control Center (RCC) which is responsible for flight safety, and for delivering captured best source telemetry to those responsible for the platform being flown. When r
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Єнотова, Марія Максимівна, and Mariia Maksymivna Yenotova. "Method of optimization of the process of managing risk factors of aviation events based on the criterion of minimum total costs." Thesis, Національний авіаційний університет, 2020. https://er.nau.edu.ua/handle/NAU/45652.

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Робота публікується згідно наказу ректора від 21.01.2020 р. №008/од "Про перевірку кваліфікаційних робіт на академічний плагіат 2019-2020р.р. навчальному році ". Керівник проекту: к.т.н., доц. Алексєєв Олег Миколайович<br>The master thesis assignment to diploma work “Method of optimization of the process of managing risk factors of aviation events based on the criterion of minimum total costs” contains 26 illustrative figures, graphs, 49 formulas and 7 tables. The object of research in the work is the airline flight safety management system. The subject of the research is a method of increa
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Nötzel, Klaus R. "Integrated Satellite Control Center." International Foundation for Telemetering, 1995. http://hdl.handle.net/10150/611618.

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International Telemetering Conference Proceedings / October 30-November 02, 1995 / Riviera Hotel, Las Vegas, Nevada<br>Deutsche Telekom has been operating different flight models for several years. A Satellite Control Center (SCC) was designed and installed to support the operation of the satellite systems DFS Kopernikus and TV-Sat. The DFS Kopernikus system is composed of three flight models and the satellite system TV-Sat has one flight model. The aim was to design an SCC and ground stations in a way, enabling the operation of satellites and groundstations by only two operators at the main c
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Rubio, Pedro, and Jesus Alvarez. "Smart Radio Control System (For Flight Test Centers)." International Foundation for Telemetering, 2015. http://hdl.handle.net/10150/596398.

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ITC/USA 2015 Conference Proceedings / The Fifty-First Annual International Telemetering Conference and Technical Exhibition / October 26-29, 2015 / Bally's Hotel & Convention Center, Las Vegas, NV<br>Among the rich infrastructure of a Telemetry/Ground Station Center dwells the subset dedicated to radio communications. Radios are mainly used to communicate with the aircraft under test in order to give guidance and feedback from ground specialists. Sometimes, however, radios themselves become the subject of the test, requiring a full set of them with all their features and capabilities (Military
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Richard, Gaetan C., and Laszlo Kiss. "NEXT GENERATION ANTENNA CONTROLLERS FOR THE NASA DRYDEN FLIGHT RESEARCH CENTER." International Foundation for Telemetering, 1996. http://hdl.handle.net/10150/608362.

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International Telemetering Conference Proceedings / October 28-31, 1996 / Town and Country Hotel and Convention Center, San Diego, California<br>Lower operating budgets and reduced personnel are causing the operators of test ranges to consolidate their assets and seek ways to maximize their utilization. This paper presents the versatile approach used by the NASA Dryden Flight Test Facility located at Edwards Air Force Base to monitor, control and operate five of its diversely located telemetry systems from a central control room. It describes a new generation of multi-purpose antenna cont
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Forshaw, Jason Leigh. "Transitioning flight guidance and control for a twin rotor tailsitter unmanned air vehicle." Thesis, University of Surrey, 2013. http://epubs.surrey.ac.uk/837960/.

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The future of aircraft lies in highly intelligent vehicles which are able to adapt themselves to different missions and take-off and land anywhere. Tailsitters, aircraft capable of controlled transitions between horizontal flight (like a fixed-wing aircraft) and vertical flight (like a rotary-wing aircraft), are one such form of vehicle. The focus of this research stems from a collaboration between the Surrey Space Centre and QinetiQ involving a new class of VTOL tailsitter - the QinetiQ Eye-On™ UAV - which offers uniqueness from all other known tailsitters in its use of twin helicopter rotors
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Lindsey, Patricia F. "A comparison of spatial interpretations of NASA's payload operations control center, Marshall Space Flight Center, using real world and virtual reality observations." Diss., This resource online, 1996. http://scholar.lib.vt.edu/theses/available/etd-11082006-133635/.

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Kegel, Thomas, Bruce Lipe, and Jacquelyn Swords. "REAL-TIME TELEMETRY DATA SUPPORT FOR THE F-22 FLIGHT TEST PROGRAM." International Foundation for Telemetering, 1999. http://hdl.handle.net/10150/607312.

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International Telemetering Conference Proceedings / October 25-28, 1999 / Riviera Hotel and Convention Center, Las Vegas, Nevada<br>This paper describes the recently developed F-22 real-time telemetry data processing system. The F-22 Combined Test Force (CTF) and the Range Division worked together to develop a real-time telemetry processing system able to support the F-22’s fast paced flight test program. This paper provides an overview of the Ridley Mission Control Center (RMCC) modernization effort for F-22. The paper also describes how the F-22 uses the Advanced Data Acquisition and Pr
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Náglová, Katarína. "Konvenční a adaptivní metody nastavení parametrů regulátoru pro řízení letové výšky letadla s pohyblivou pozicí těžiště v prostředí MATLAB - Simulink." Master's thesis, Vysoké učení technické v Brně. Fakulta elektrotechniky a komunikačních technologií, 2013. http://www.nusl.cz/ntk/nusl-219931.

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The thesis is focused on aircraft flight level control in case when the location of center of gravity changes during flight. The theoretical part of the thesis describes basics of aerodynamics, which are necessary to understand airplane's behavior and its control theory. Basics of state theory and stability of systems, as it is used for design of linear model. This part also mentions mathematical equations of nonlinear model of business jet and discusses conventional and adaptive methods used to design autopilot parameters. Several autopilots were designed in practical part of the thesis. The
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Books on the topic "Flights control center"

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Center, Goddard Space Flight, ed. The Network Control Center. National Aeronautics and Space Administration, Goddard Space Flight Center, 1991.

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P, Latyshev V., Sorokoletova N. A, Nechaev V. I, Svirskiĭ S. P, and Artemov E. N, eds. T͡s︡entr upravlenii͡a︡ poletami =: Spaceflights Control Centre. "Mashinostroenie", 1990.

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Carter, John. Initial flight test of the production support flight control computers at NASA Dryden Flight Research Center. National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

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Carter, John. Initial flight test of the production support flight control computers at NASA Dryden Flight Research Center. National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

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F, Carter John. Initial flight test of the production support flight control computers at NASA Dryden Flight Research Center. National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

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Flight Mechanics Symposium (1997 Goddard Space Flight Center). Flight Mechanics Symposium 1997: Proceedings of a conference sponsored by NASA Goddard Space Flight Center at Goddard Space Flight Center, Greenbelt, Maryland, May 19-21, 1997. Edited by Walls Donna M, Goddard Space Flight Center, and United States. National Aeronautics and Space Administration. National Aeronautics and Space Administration, 1997.

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M, Walls Donna, and Goddard Space Flight Center, eds. Flight mechanics symposium 1997: Proceedings of a conference sponsored by NASA Goddard Space Flight Center at Goddard Space Flight Center, Greenbelt, Maryland, May 19-21, 1997. National Aeronautics and Space Administration, Goddard Space Flight Center, 1997.

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Hartman, Kathy R. Flight mechanics/ estimation theory symposium 1995 ; proceedings of a symposium sponsored by NASA Goddard Space Flight Center at Goddard Space Flight Center, Greenbelt, Maryland, May 16-18, 1995. Goddard Space Flight Center, 1995.

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Stengle, Thomas H. Flight Mechanics/Estimation Theory Symposium 1992: Proceedings of a symposium sponsored by NASA Goddard Space Flight Center and held at Goddard Space Flight Center, Greenbelt, Maryland, May 5-7, 1992. Edited by Goddard Space Flight Center and Flight Mechanics/Estimation Theory Symposium (1992 : Greenbelt, Md.). Goddard Space Flight Center, 1993.

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M, Green Steven, and Langley Research Center, eds. Flight evaluation of Center-TRACON Automation System trajectory prediction process. National Aeronautics and Space Administration, Langley Research Center, 1998.

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Book chapters on the topic "Flights control center"

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Lazarevic, Aleksandar. "Data Mining for Intrusion Detection." In Data Warehousing and Mining. IGI Global, 2008. http://dx.doi.org/10.4018/978-1-59904-951-9.ch183.

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Today computers control power, oil and gas delivery, communication systems, transportation networks, banking and financial services, and various other infrastructure services critical to the functioning of our society. However, as the cost of the information processing and Internet accessibility falls, more and more organizations are becoming vulnerable to a wide variety of cyber threats. According to a recent survey by CERT/CC (Computer Emergency Response Team/Coordination Center), the rate of cyber attacks has been more than doubling every year in recent times (Figure 1). In addition, the se
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Polyakhova, Elena, and Vladimir Korolev. "Astrodynamics in Photogravitational Field of the Sun: Space Flights with a Solar Sail." In Gravitational Field [Working Title]. IntechOpen, 2022. http://dx.doi.org/10.5772/intechopen.102005.

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Mathematical models of the controlled motion of a spacecraft with a solar sail and the possibilities are considered, taking into account the translational motion in the gravitational field, the forces of light pressure, and rotational motion relative to the center of mass. The structure of possible problems of photogravitational celestial mechanics is proposed. To control movement, it is possible to change the size, shape, surface properties, and orientation of the elements of the sail system in relation to the flow of sunlight. The equations of motion can be presented on the basis of the prob
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Fant, Clyde E., and Mitchell G. Reddish. "Cos." In A Guide to Biblical Sites in Greece and Turkey. Oxford University Press, 2003. http://dx.doi.org/10.1093/oso/9780195139174.003.0014.

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Cos, home of Hippocrates, the father of modern medicine, is the third largest island of the Dodecanese (Twelve Islands). In antiquity its population was 120,000, eight times that of today. Its fame derived from the renowned Asclepeion of Cos, a healing center and religious shrine devoted to Asclepius, the god of healing. Tourists still come to marvel at this spectacular architectural structure, and international medical conferences are conducted on the island in memory of Hippocrates. Cos (also spelled Kos) lies only 3 miles off the coast of Turkey, near the Bodrum peninsula. Connections are a
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M. Lam, Quang, Anthony J. Calise, and Nhan T. Nguyen. "Perspective Chapter: Intelligent Adaptive Flight Control Augmentation of a Dynamic Inversion Autopilot." In Latest Adaptive Control Systems [Working Title]. IntechOpen, 2024. http://dx.doi.org/10.5772/intechopen.1004113.

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High-speed UAV flight control is challenged by unknown external aerodynamic disturbances and internal system variations due to complex aerodynamic configuration, propellant consumption, the center of gravity movement, and possible actuator failures. Redundant aerodynamic control effectors and engine inlet control mechanisms are exploited/blended to maintain adequate force/moment control to satisfy flight control reliability requirements. A control allocation (CA) mixing matrix is an essential element of the redundancy design in addressing fault tolerance capabilities. This paper employs an Int
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"John Glenn’s Official Communication with the Command Center." In Milestone Documents in American History. Schlager Group Inc., 2020. https://doi.org/10.3735/9781935306528.book-part-138.

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On February 20, 1962, Marine Lieutenant Colonel John Glenn became the first American to orbit the earth in a space capsule. His official communication with the National Aeronautics and Space Administration’s Mission Control center at Cape Canaveral, Florida, recorded his skillful manual piloting of his capsule, Friendship 7, after the autopilot device failed during reentry. In addition, after the second orbit, the heat shield, designed to prevent the capsule from burning up during reentry, was reported to be loose. In spite of these obstacles, Glenn was able to orbit the earth three times and
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Dyson, Freeman J. "The High Road." In The Sun, the Genome, & the Internet. Oxford University PressNew York, NY, 2000. http://dx.doi.org/10.1093/oso/9780195139228.003.0003.

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Abstract In 1985 I was visiting the Johnson Space Flight Center in Houston and climbing around in the space shuttle that they keep there for visitors to examine. That was before the Challenger disaster, when the shuttle was advertised as a safe ride for congressmen and schoolteachers. What impressed me about the shuttle was the immense quantity of §ruff that they had on board for the care and comfort of human passengers. It felt more like a hotd or a hospital than a rocketship. I made rough calculations of how many tons of §ruff they were flying to keep seven passengers alive and well for a co
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Khalid, S. "Optimizing Airspace Management During Space Launches." In Advances in Mechatronics and Mechanical Engineering. IGI Global, 2024. https://doi.org/10.4018/979-8-3693-6035-4.ch008.

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This chapter addresses the challenges posed by increasing space launches on air traffic management, proposing strategies to optimize airspace efficiency while maintaining safety. Key issues include large airspace blockages, extended closure windows, and limited situational awareness in oceanic environments. The proposed solutions involve implementing dynamic, geographically limited airspace closures using Flexible Use of Airspace principles. A three-stage pre-launch roadmap identifies affected air routes, determines separation distances, and creates alternative paths. Post-launch analysis meth
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KIM, SUNGWAN. "MINIMAL TIME CHANGE DETECTION ALGORITHM FOR RECONFIGURABLE CONTROL SYSTEM AND APPLICATION TO AEROSPACE**This work was supported by NASA Ames Research Center, DFRF through UCLA Flight Systems Research Center(FSRC), Grant Number NCC 2-374." In Automatic Control in Aerospace 1994 (Aerospace Control '94). Elsevier, 1995. http://dx.doi.org/10.1016/b978-0-08-042238-1.50045-8.

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Zhang, Yueping, and Yiming He. "Research on Construction Technology of Multi-Airport Collaborative Flight Command and Control Based on Data Center." In Frontiers in Artificial Intelligence and Applications. IOS Press, 2025. https://doi.org/10.3233/faia250192.

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As more airports/bases are gradually coming into use, three or more airports/bases will simultaneously carry out various activities, with scenarios becoming increasingly complex. These changes in scenarios require the command automation systems at each airport to coordinate and manage tasks across multiple airports under the “one airspace, multiple airports” model, enabling situation awareness, data centers, and collaborative command among multiple systems. To meet the needs of multi-airport command, research is proposed on the construction technology for multi-airport collaborative command an
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Maar, Henry Richard. "The Lost Years." In Freeze! Cornell University Press, 2022. http://dx.doi.org/10.7591/cornell/9781501760884.003.0002.

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This chapter charts the trajectory of the peace movement from the Vietnam War to the Nuclear Weapons Freeze Campaign. In an era where the New Right was taking center stage, peace activists pushed back on the escalating arms race while making the question of war and peace central to US politics. Thus, in these lost years, activists sought to launch a peace conversion campaign as the answer to US militarism, for which Vietnam was only a symptom. Amid conflicting activist goals and agendas, it would take a new idea from an outsider to unite peace activists. The chapter then looks at the Stop the
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Conference papers on the topic "Flights control center"

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Zimmermann, Michael, Stephanus Klasen, Martin Gestwa, and Andreas Lederle. "Avoiding Obstacles during Approach: DVE-Mitigation Flight Trials and Beyond." In Vertical Flight Society 74th Annual Forum & Technology Display. The Vertical Flight Society, 2018. http://dx.doi.org/10.4050/f-0074-2018-12732.

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Helicopter landings on unprepared sites can quickly become a challenging task. Especially when environmental factors reduce the available visual cues for the pilot, the risk of disorientation increases. Motivated by avoiding accidents during helicopter approaches, a novel pilot assistance system was developed by a workgroup from the German Aerospace Center (DLR) and HENSOLDT Sensors GmbH. The research system combines 3D conformal tunnel-in-the-sky symbology with dynamic path updates driven by a laser sensor. In early 2017, the system was evaluated in flight using DLR's research rotorcraft Acti
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Brown, Robert. "System Identification of a Free-Flying Quadrotor in a Wind Tunnel using Motion Capture Feedback." In Vertical Flight Society 80th Annual Forum & Technology Display. The Vertical Flight Society, 2024. http://dx.doi.org/10.4050/f-0080-2024-1220.

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A system identification study was conducted on a quadrotor unmanned aerial system (UAS) that was free-flying inside the test section of the Naval Surface Warfare Center Carderock Division's Subsonic Wind Tunnel. Motion capture cameras installed in the wind tunnel provided position feedback information to the aircraft in real time, enabling autonomous flights. Longitudinal, lateral, heave, and yaw axis frequency sweeps were conducted at airspeeds up to 20 knots, in 5 knot increments. The extracted flight dynamics model showed excellent agreement in both the time and frequency domains across all
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Simmons, Benjamin, Kasey Ackerman, Garrett Asper, et al. "Subscale Tiltrotor eVTOL Aircraft Dynamic Modeling and Flight Control Software Development." In Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society, 2025. https://doi.org/10.4050/f-0081-2025-161.

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This paper describes the dynamic modeling and flight control software development efforts for a subscale tiltrotor electric vertical takeoff and landing (eVTOL) aircraft built at NASA Langley Research Center. The vehicle, referred to as the Research Aircraft for eVTOL Enabling techNologies (RAVEN) SubscaleWind-Tunnel and Flight Test (SWFT) model, serves as a flight dynamics and controls research testbed to foster advances in eVTOL aircraft technology. After fabricating the vehicle, wind-tunnel testing was conducted to identify a high-fidelity aero-propulsive model for use in a flight dynamics
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Agrawal, Shivansh, Kyle Collins, Patric Hruswicki, and Syed Zuhair. "Handling Qualities Analysis of a Large Multi-Rotor eVTOL using RPM, Collective and Cyclic Control Allocation Methods." In Vertical Flight Society 80th Annual Forum & Technology Display. The Vertical Flight Society, 2024. http://dx.doi.org/10.4050/f-0080-2024-1299.

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The Eagle Flight Research Center (EFRC) at Embry-Riddle Aeronautical University (ERAU) is investigating the handling qualities of partial and full rotor failure modes of a multi-rotor vehicle testbed employing Distributed Electric Propulsion (DEP) systems intended for Advanced Air Mobility (AAM) vehicles. In order to pave the way for commercial operations, the AAM industry requires a deeper understanding of the handling characteristics and the vehicle's dynamics and controllability under rotor failure conditions. The objective of the research performed at the EFRC centered around designing and
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Hodges, Todd, Susan Gorton, and Karen Jackson. "Historical Contributions to Vertical Flight at the NASA Langley Research Center." In Vertical Flight Society 72nd Annual Forum & Technology Display. The Vertical Flight Society, 2016. http://dx.doi.org/10.4050/f-0072-2016-11334.

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The NASA Langley Research Center has had a long and distinguished history in powered lift technology development. This research has formed the foundation of knowledge for the powered lift community worldwide. From aerodynamics to structures, aeromechanics, powered lift, acoustics, materials, stability &amp; control, structural dynamics and human factors, Langley has made significant contributions to the advancement of vertical lift technologies. This research has encompassed basic phenomenological studies through subscale laboratory testing, analytical tool development, applied demonstrations
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van, Berend, Ganesh Rajagopalan, Sung Jung, Marc Wentrup, and Jianping Yin. "A Simple Analytical Model for Investigation of Fuselage-Rotor Interference." In Vertical Flight Society 72nd Annual Forum & Technology Display. The Vertical Flight Society, 2016. http://dx.doi.org/10.4050/f-0072-2016-11491.

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A simple analytical model to account for fuselage-induced velocities at rotor blade elements and at rotor wake nodes is described. The method is applied to four different fuselage configurations: two rotor test rig bodies used in the NASA Ames Full-Scale Aerodynamics Complex and two test rigs used by the DLR (German Aerospace Center) in the Large Low-speed Facility of the German-Dutch Wind tunnels in the Netherlands. The fuselage-induced flow fields in the volume of rotor operation above the respective fuselages are modeled in the range of angle of attack and sideslip applicable in the respect
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Mitchell, Dave, Sean Roark, and Gino Molinaro. "A Portable Display for Evaluating Handling Qualities in Shipboard Hover." In Vertical Flight Society 70th Annual Forum & Technology Display. The Vertical Flight Society, 2014. http://dx.doi.org/10.4050/f-0070-2014-9507.

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A limited flight test assessment of a portable display for evaluating handling qualities in shipboard hover was performed. The Portable Optical Navigation Guidance (PONG) display is intended as a land-based component for replicating the control motions required for hovering over the deck of a small ship. It is based on the Canadian National Research Council's Flight Research Laboratory's Superslide display. A U.S. Marine Corps fleet-configured Bell UH-1N, used by the U.S. Naval Air Warfare Center's Naval Aviation Center for Rotorcraft Advancement organization, was flown by three pilots, all wi
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D., Robert, and Gerardo Nuñez. "Low-Speed Wind Tunnel Drag Test of a 2/5 Scale AH-56 Cheyenne Door-Hinge Hub." In Vertical Flight Society 73rd Annual Forum & Technology Display. The Vertical Flight Society, 2017. http://dx.doi.org/10.4050/f-0073-2017-12181.

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The Aviation Development Directorate of the U.S. Army Aviation and Missile Research, Development and Engineering Center (AMRDEC) conducted a drag test of a non-rotating 2/5 scale Lockheed AH-56 Cheyenne main rotor hub in the U.S. Army 7- by 10-foot Wind Tunnel located at NASA Ames Research Center in Moffett Field, CA. The purpose of the test was to quantify the drag reduction on the Cheyenne's unique "door-hinge" style hub when the mechanical control gyro is removed, with the implicit assumption that the control and stabilization functions of the gyro could be replaced by a modern flight contr
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Chernak, Harry, Kyle Collins, Kranthi Kumar Deveerasetty, Patric Hruswicki, and Syed Zuhair Ali Razvi. "Development and Evaluation of a Quad-Heli eVTOL Capable of Safe Fly with a Failed Rotor." In Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society, 2025. https://doi.org/10.4050/f-0081-2025-133.

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With advanced air mobility (AAM) vehicles becoming an increasingly popular topic in aviation, the Eagle Flight Research Center (EFRC) at Embry-Riddle Aeronautical University continues to investigate control strategies that enhance aircraft resilience to total power unit failures. Utilizing a distributed electric propulsion (DEP) quad-heli test bed, the EFRC has explored a variety of control laws and hardware configurations to evaluate their effectiveness under failure conditions, including sustained flight with a completely inoperative rotor. The aircraft utilizes a fractional-order PID (FOPID
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Halder, Atanu, and Moble Benedict. "Nonlinear Aeroelastic Coupled Trim Analysis of a Cyclocopter in Hover." In Vertical Flight Society 73rd Annual Forum & Technology Display. The Vertical Flight Society, 2017. http://dx.doi.org/10.4050/f-0073-2017-12050.

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In this paper, detailed development of a nonlinear aeroelastic coupled trim model of a twin-cyclocopter, consisting of two cycloidal rotors (also known as cyclorotors) as main rotors and a conventional horizontal tail-rotor for anti-pitch torque and control, is presented. Coupled trim analysis requires simultaneous computation of trim controls, vehicle orientation and blade structural responses so that both blade response equations and vehicle trim equations are satisfied. To obtain the blade structural response and the hub loads in the vehicle frame for the cyclorotors, a nonlinear aeroelasti
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Reports on the topic "Flights control center"

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Sheppard, Jeffrey A. Options for Organizing the Tanker Airlift Control Center Flight Dispatch Function: An Exploratory Concept Study. Defense Technical Information Center, 2000. http://dx.doi.org/10.21236/ada430858.

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