Relevant bibliographies by topics / Flight dynamics

Contents

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

Academic literature on the topic 'Flight dynamics'

Author: Grafiati
Published: 4 June 2021
Last updated: 25 July 2025

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Journal articles on the topic "Flight dynamics"

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Philip, Scott Blackwelder. "UAV Flight Dynamics." International Journal of Aeronautical Science & Aerospace Research 2, no. 6 (2015): 81–85. https://doi.org/10.19070/2470-4415-150009.

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In the interest of promoting the integration of hybrid-electric power train into the aviation industry, research is being conducted by North Carolina State University to establish the feasibility of electrified power train in a small scale unmanned aerial vehicle (UAV). To accomplish this, it is first necessary to understand dynamics of the system to calculate the required power associated with each portions of the aircraft’s mission. Though research that has been conducted in the past based power required on published governing equations. However, in the interest of under
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Tian, Xian Ke, Shuo Tang, and Qiang Jun Zhu. "Flight Dynamics Modeling and Analysis of Flexible Hypersonic Flight Vehicles." Applied Mechanics and Materials 275-277 (January 2013): 513–17. http://dx.doi.org/10.4028/www.scientific.net/amm.275-277.513.

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Facing the difficulty of flight dynamics modeling about flexible hypersonic flight vehicles, from view on the Lagrange’s equations based on dynamic first principle, this paper firstly developed kinetic energy and flexibility potential energy of the vehicle, then achieved concise flight dynamics equations by quasi-coordinates which could fully include coupling characteristics of flight dynamics, and lastly made necessary analysis about the equations. The result of study illustrates that flight dynamics equations of flexible hypersonic flight vehicles based on quasi-coordinates can satisfy the r
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Laurence III, Roger J., and Brian M. Argrow. "Numerical Calibration of a Low-Speed sUAS Flush Air Data System." Journal of Atmospheric and Oceanic Technology 36, no. 8 (2019): 1577–90. http://dx.doi.org/10.1175/jtech-d-18-0208.1.

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AbstractA method using computational fluid dynamics to numerically calibrate a flush air data system is presented. A small unmanned aircraft system (sUAS) has been equipped with a flush air data system and experimentally tested. The flush air data system uses computational fluid dynamics to train neural networks and is validated using the in-flight data that were previously collected. Results of the flight validation are presented, along with ways to improve the accuracy of the system. Several different calibration approaches are presented and compared with each other. The best-case results wi
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Cook, M. V. "Dynamics of Flight." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 211, no. 2 (1997): 129–30. http://dx.doi.org/10.1177/095441009721100202.

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Bai, Ye, and Srikanth Gururajan. "Evaluation of a Baseline Controller for Autonomous “Figure-8” Flights of a Morphing Geometry Quadcopter: Flight Performance." Drones 3, no. 3 (2019): 70. http://dx.doi.org/10.3390/drones3030070.

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This article describes the design, fabrication, and flight test evaluation of a morphing geometry quadcopter capable of changing its intersection angle in-flight. The experiments were conducted at the Aircraft Computational and Resource Aware Fault Tolerance (AirCRAFT) Lab, Parks College of Engineering, Aviation and Technology at Saint Louis University, St. Louis, MO. The flight test matrix included flights in a “Figure-8” trajectory in two different morphing configurations (21° and 27°), as well as the nominal geometry configuration, two different flight velocities (1.5 m/s and 2.5 m/s), two
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Lu, Ke, Chunsheng Liu, Chunhua Li, and Renliang Chen. "Flight Dynamics Modeling and Dynamic Stability Analysis of Tilt-Rotor Aircraft." International Journal of Aerospace Engineering 2019 (August 14, 2019): 1–15. http://dx.doi.org/10.1155/2019/5737212.

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The tilt-rotor aircraft has often been proposed as a means to increase the maximum speed of the conventional helicopter. The tilt-rotor aircraft consists of three primary flight modes that are the helicopter flight mode in low forward speed flight, airplane flight mode in high forward speed flight, and conversion flight mode. The aim of this paper is to develop a nonlinear flight dynamics mathematical modeling method of tilt-rotor aircraft and investigate the dynamic stability characteristics of tilt-rotor aircraft. First, a nonlinear tilt-rotor aircraft flight dynamics model is developed. The
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Ibrahim, Noureldein A., Mohamed Y. Zakaria, and Ashraf M. Kamal. "Simulation of tilt-rotor UAV flight dynamics in horizontal flight." Journal of Physics: Conference Series 2616, no. 1 (2023): 012006. http://dx.doi.org/10.1088/1742-6596/2616/1/012006.

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Abstract Tilt-rotor unmanned aerial vehicles (UAV) have gained significant importance in the aeronautical industry due to their ability to transition between vertical and horizontal flight. One of the important steps in the development of such UAVs is to assess their performance and stability characteristics. Simulation of flight dynamics is an essential tool that enables the designers to test and optimize the flight characteristics of these UAVs. This paper presents a complete procedure for developing a 6-degree-of-freedom flight dynamics model of a tilt-rotor UAV in fixed-wing mode using a p
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SUZUKI, Kosuke, Masaya KOUJI, and Masato YOSHINO. "Flight dynamics in forward flights of cabbage white butterfly." Journal of Fluid Science and Technology 18, no. 1 (2023): JFST0011. http://dx.doi.org/10.1299/jfst.2023jfst0011.

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Smith, Kevin M. "Aerodynamic Essentials for Crew Station Design Teams." International Journal of Aviation Systems, Operations and Training 2, no. 1 (2015): 1–20. http://dx.doi.org/10.4018/ijasot.2015010101.

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Increasing emphasis is being placed on various aspects of flight dynamics in aviation. This includes such things as upset and stall recovery, wind shear recovery, and approach instability recovery. Operators, safety analysts, and designers are now actively discussing “dynamic situation awareness.” Because of this, there is the need to understand the dynamic nature of flight operations, and incorporate this understanding in state-of-the-art flight deck systems and training programs. This article offers designers, operators, and trainers a quick review of some of the most important aspects of fl
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Shamliev, Alexander, Peter Mitrouchev, and Maya Dimitrova. "Atmospheric Boundary Layer Dynamics Evaluation Using Piezo-Resistive Technology for Unpowered Areal Vehicles." International Journal of Cyber-Physical Systems 2, no. 1 (2020): 1–19. http://dx.doi.org/10.4018/ijcps.2020010101.

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The paper presents a method for real-time observing of the convectional processes in the atmosphere boundary layer. The essence of the method is in providing real-time measurement of temperature, humidity, and pressure during the flight of a glider (soaring flight). Based on these measurements, a real-time evaluation of the atmosphere dynamics is presented. Measurements are taken during soaring flight of the glider and during the flight of a remotely controlled quadrocopter. Additionally, a method for atmosphere thermal identification by the measured parameters is introduced. The main applicat
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Dissertations / Theses on the topic "Flight dynamics"

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Benedetti, Diego Muniz. "Paragliders flight dynamics." Universidade Federal de Minas Gerais, 2012. http://hdl.handle.net/1843/BUOS-95RGS5.

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Paragliding has become popular in the last three decades, and the development of modern paragliders has shown considerable improvements on performance and safety. However, due to the sportive purpose of paragliders, scientific studies on this subject are still rare. The achievements on paragliders design are mostly originated from industry, and, although there are many manufactures with years of experience designing paragliders, it cannot be found in the available literature works dedicated on paragliders design theory. Taking in account the lack of specific information about paragliders engin
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Shankar, Kumar Priya Balaji. "Dynamics of spacecraft formation flight." Thesis, University of Southampton, 2005. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.417979.

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Pagliuca, Giampaolo. "Model reduction for flight dynamics using computational fluid dynamics." Thesis, University of Liverpool, 2018. http://livrepository.liverpool.ac.uk/3029018/.

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The coupling of computational fluid dynamics and rigid body dynamics promises enhanced multidisciplinary simulation capability for aircraft design and certification. Industrial application of such coupled simulations is limited however by computational cost. In this context, model reduction can retain the fidelity of the underlying model while decreasing the overall computational effort. Thus, investigation of such coupled model reduction is presented in this thesis. The technique described herein relies on an expansion of the full order non-linear residual function in a truncated Taylor serie
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Montalvo, Carlos. "Meta aircraft flight dynamics and controls." Diss., Georgia Institute of Technology, 2014. http://hdl.handle.net/1853/51854.

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The field of mobile robotic systems has become a rich area of research and design. These systems can navigate difficult terrain using multiple actuators with conventional ambulation, by hopping, jumping, or for aerial vehicles, using flapping wings, propellers, or engines to maintain aerial flight. Unmanned Aerial Systems(UAS) have been used extensively in both military and civilian applications such as reconnaissance or search and rescue missions. For air vehicles, range and endurance is a crucial design parameter as it governs which missions can be performed by a particular vehicle. In addit
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Seigler, Thomas Michael. "Dynamics and Control of Morphing Aircraft." Diss., Virginia Tech, 2005. http://hdl.handle.net/10919/28681.

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The following work is directed towards an evaluation of aircraft that undergo structural shape change for the purpose of optimized flight and maneuvering control authority. Dynamical equations are derived for a morphing aircraft based on two primary representations; a general non-rigid model and a multi-rigid-body. A simplified model is then proposed by considering the altering structural portions to be composed of a small number of mass particles. The equations are then extended to consider atmospheric flight representations where the longitudinal and lateral equations are derived. Two aspect
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Zaludin, Zairil A. "Flight dynamics and automatic flight control system of an hypersonic transport aircraft." Thesis, University of Southampton, 1999. https://eprints.soton.ac.uk/47120/.

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Leonard, Benjamin Yoshi. "Flapping Wing Flight Dynamic Modeling." Thesis, Virginia Tech, 2011. http://hdl.handle.net/10919/34790.

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Highly agile, hover capable flapping wing flight is a relatively new area of study in engineering. Researchers are looking to flapping flight as a potential source for the next generation of reconnaissance and surveillance vehicles. These systems involve highly complicated physics surrounding the flapping wing motion and unusual characteristics due to a hover requirement not normally associated with conventional aircraft. To that end this study focuses on examining the various models and physical parameters that are considered in various other studies. The importance of these models is conside
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Kabaliuk, Natalia. "Dynamics of Blood Drop Formation and Flight." Thesis, University of Canterbury. Mechanical Engineering, 2014. http://hdl.handle.net/10092/8979.

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Violent crimes involving bloodshed may result in the formation of a number of blood drops that move through air and impact onto a surface producing a bloodstain pattern. Bloodstain Pattern Analysis (BPA), the analysis of the position, distribution, size and morphology of the stains within the pattern present at a crime scene, may provide information about the events that gave rise to the bloodshed. The location of blood origin, i.e. victim’s position at the moment of wounding and (or) wound location, determination is of major interest to BPA. This study investigated the dynamics of formation a
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Watkiss, Eric John. "Flight dynamics of an unmanned aerial vehicle." Thesis, Monterey, California. Naval Postgraduate School, 1994. http://hdl.handle.net/10945/28222.

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Approved for public release; distribution is unlimited.<br>Moments of inertia were experimentally determined and longitudinal and lateral/directional static and dynamic stability and control derivatives were estimated for a fixed wing Unmanned Air Vehicle (UAV). Dynamic responses to various inputs were predicted based upon the estimated derivatives. A divergent spiral mode was revealed, but no particularly hazardous dynamics were predicted. The aircraft was then instrumented with an airspeed indicator, which when combined with the ability to determine elevator deflection through trim setting o
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Charles, Guy Alexander. "Bifurcation tailoring applied to nonlinear flight dynamics." Thesis, University of Bristol, 2003. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.274630.

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Books on the topic "Flight dynamics"

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Padfield, Gareth D., ed. Helicopter Flight Dynamics. John Wiley & Sons, Ltd, 2018. http://dx.doi.org/10.1002/9781119401087.

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Padfield, Gareth D., ed. Helicopter Flight Dynamics. Blackwell Publishing Ltd, 2007. http://dx.doi.org/10.1002/9780470691847.

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Abzug, Malcolm J. Computational flight dynamics. American Institute of Aeronautics and Astronautics, 1998.

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Roskam, Jan. Airplane flight dynamics and automatic flight controls. Design, Analysis and Research Corporation, 1995.

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Roskam, Jan. Airplane flight dynamics and automatic flight controls. Design, Analysis and Research Corporation, 1995.

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Roskam, Jan. Airplane flight dynamics and automatic flight controls. Roskam Aviation and Engineering Corp., 1994.

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Sinha, Nandan K., and N. Ananthkrishnan. Advanced Flight Dynamics with Elements of Flight Control. CRC Press, 2017. http://dx.doi.org/10.1201/9781315151977.

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Yihua, Cao. Principles of helicopter flight dynamics. Coxmoor, 2009.

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Schmidt, Louis V. Introduction to aircraft flight dynamics. American Institute of Aeronautics and Astronautics, 1998.

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Wu, Chi-Heng. Flight dynamics of a flexible aircraft. Shaker, 1999.

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Book chapters on the topic "Flight dynamics"

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Polyakhov, Nikolai Nikolaevich, and Mikhail Petrovich Yushkov. "Flight Dynamics." In Foundations of Engineering Mechanics. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-64118-4_10.

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DeLaurier, James. "Flight Dynamics." In Aircraft Design Concepts. CRC Press, 2022. http://dx.doi.org/10.1201/9781315228167-6.

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Cai, Guowei, Ben M. Chen, and Tong Heng Lee. "Flight Dynamics Modeling." In Advances in Industrial Control. Springer London, 2011. http://dx.doi.org/10.1007/978-0-85729-635-1_6.

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Griebel, Hannes. "Flight Dynamics Analysis." In Reaching High Altitudes on Mars with an Inflatable Hypersonic Drag Balloon (Ballute). Vieweg+Teubner, 2011. http://dx.doi.org/10.1007/978-3-8348-9911-8_5.

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Sinha, Nandan K., and N. Ananthkrishnan. "Longitudinal Flight Dynamics." In Advanced Flight Dynamics with Elements of Flight Control. CRC Press, 2017. http://dx.doi.org/10.1201/9781315151977-4.

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Sinha, Nandan K., and N. Ananthkrishnan. "Computational Flight Dynamics." In Elementary Flight Dynamics with an Introduction to Bifurcation and Continuation Methods, 2nd ed. CRC Press, 2021. http://dx.doi.org/10.1201/9781003096801-8.

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"Front Matter." In Flight Dynamics. Princeton University Press, 2015. http://dx.doi.org/10.2307/j.ctt1287kgx.1.

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"Coupled Longitudinal and Lateral-Directional Motions." In Flight Dynamics. Princeton University Press, 2015. http://dx.doi.org/10.2307/j.ctt1287kgx.10.

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"Epilogue." In Flight Dynamics. Princeton University Press, 2015. http://dx.doi.org/10.2307/j.ctt1287kgx.11.

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"Appendix A." In Flight Dynamics. Princeton University Press, 2015. http://dx.doi.org/10.2307/j.ctt1287kgx.12.

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Conference papers on the topic "Flight dynamics"

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Gennaretti, Massimo, Roberto Celi, Claudio Pasquali, Felice Cardito, Jacopo Serafini, and Giovanni Bernardini. "Dynamic Wake Inflow Modeling in Ground Effect for Flight Dynamics Applications." In Vertical Flight Society 73rd Annual Forum & Technology Display. The Vertical Flight Society, 2017. http://dx.doi.org/10.4050/f-0073-2017-12059.

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Rotor dynamic wake inflow modeling is one of the main issues in the development of efficient and reliable tools for design and flight dynamic simulation of rotorcraft. In general, it is affected by the operating condition (hovering, advancing, steady or maneuvering flight), but the interference with external obstacles might play a crucial role, especially during landing or close-to-ground procedures. The aim of this paper is the presentation of a LTI, finite-state model for the prediction of dynamic wake inflow of helicopter rotors in ground effect. First, two high-fidelity boundary-element ae
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Talluri, Geetam, and Anand Konjengbam. "Digital Twin-based Flight Dynamics Simulation." In 2024 IEEE Conference on Engineering Informatics (ICEI). IEEE, 2024. https://doi.org/10.1109/icei64305.2024.10912412.

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Beck, Roger, and Wayne Durham. "Flight simulation in flight dynamics education." In 24th Atmospheric Flight Mechanics Conference. American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-4261.

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Zipfel, Peter. "Tensor Flight Dynamics." In AIAA Atmospheric Flight Mechanics Conference. American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-6725.

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Vassberg, John. "Boomerang Flight Dynamics." In 30th AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 2012. http://dx.doi.org/10.2514/6.2012-2650.

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SCHMIDT, EDWARD. "Segmented penetrator flight dynamics." In Flight Simulation and Technologies. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-3652.

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Levi, Joshua, Karen Richon, Ann Nicholson, and Jonathan Landis. "The JWST Flight Dynamics Operations Concept and Flight Dynamics Ground System." In 2020 IEEE Aerospace Conference. IEEE, 2020. http://dx.doi.org/10.1109/aero47225.2020.9172797.

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Foust, Rebecca, Benjamin Schilling, Lev Rodovskiy, et al. "Dragonfly First Flight – Preliminary Flight Dynamics Analysis." In AIAA SCITECH 2024 Forum. American Institute of Aeronautics and Astronautics, 2024. http://dx.doi.org/10.2514/6.2024-2119.

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CULICK, FRED. "Application of dynamical systems theory to nonlinear aircraft dynamics." In 15th Atmospheric Flight Mechanics Conference. American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-4372.

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Lin, Guo-Feng, C. Lan, Jay Brandon, Guo-Feng Lin, C. Lan, and Jay Brandon. "A generalized dynamic aerodynamic coefficient model for flight dynamics applications." In 22nd Atmospheric Flight Mechanics Conference. American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-3643.

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Reports on the topic "Flight dynamics"

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Streby, Gary D. Research in Flight Dynamics. Defense Technical Information Center, 1990. http://dx.doi.org/10.21236/ada226123.

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Wenxuan, Zhu. Methods of Guidance Flight Dynamics. Defense Technical Information Center, 1991. http://dx.doi.org/10.21236/ada254248.

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Jianping, Yuan. Satellite Positioning System and Flight Dynamics,. Defense Technical Information Center, 1995. http://dx.doi.org/10.21236/ada300160.

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Jenkins, Jerry E., Gregory A. Addington, Phillip S. Beran, Deborah S. Grismer, and Ernest S. Hanff. Dynamics of Aerospace Vehicles -- Nonlinear Flight Mechanics. Defense Technical Information Center, 2000. http://dx.doi.org/10.21236/ada380300.

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Bolender, Michael A., and David B. Doman. Flight Path Angle Dynamics of Air-Breathing Hypersonic Vehicles. Defense Technical Information Center, 2005. http://dx.doi.org/10.21236/ada444974.

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Johnson, James R. Flight Dynamics Directorate (FDD) Research and Development for Aging Aircraft. Defense Technical Information Center, 1994. http://dx.doi.org/10.21236/ada361159.

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Weinacht, Paul. Prediction of Projectile Performance, Stability, and Free-Flight Motion Using Computational Fluid Dynamics. Defense Technical Information Center, 2003. http://dx.doi.org/10.21236/ada417123.

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Blair, Peter. Beyond Racial Attitudes: The Role of Outside Options in the Dynamics of White Flight. National Bureau of Economic Research, 2023. http://dx.doi.org/10.3386/w31136.

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Qin, Hantang, Beiwen Li, and Iris Rivero. In-situ Nondestructive Evaluation of In-flight Particle Dynamics and Intrinsic Properties for Directed Energy Deposition. Office of Scientific and Technical Information (OSTI), 2021. http://dx.doi.org/10.2172/1897194.

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Lee, R. S., J. Colvin, A. Frank, L. Fried, and J. Reaugh. Final report: flight dynamics and impact characteristics of thin flyer plates driven by laser-and electrically-produced plasmas. Office of Scientific and Technical Information (OSTI), 2001. http://dx.doi.org/10.2172/15006442.

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