Relevant bibliographies by topics / High speed maneuver

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

Academic literature on the topic 'High speed maneuver'

Author: Grafiati
Published: 25 May 2024
Last updated: 31 July 2025

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Journal articles on the topic "High speed maneuver"

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Kushwaha, Atul Kumar. "Design and Fabrication of Four Mode in Four-Wheeler Steering Mechanism." International Journal for Research in Applied Science and Engineering Technology 13, no. 4 (2025): 5955–87. https://doi.org/10.22214/ijraset.2025.69452.

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Abstract: Nowadays, the every vehicle existed mostly still using the two wheel steering system to control the movement of the vehicle whether it is front wheel drive, rear wheel drive or all-wheel drive. But due to the awareness of safety, four wheel steering vehicles are being used increasingly due to high performance and stability that they bring to the vehicles. In this report, the performance of four wheels steered vehicle model is considered which is optimally controlled duringalanechangemaneuverinthreetypeofconditionwhichislowspeed maneuver, medium speed maneuver and high speed maneuver.
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Li, Hao, Yuping Li, Zhongliang Zhao, Xiaobing Wang, Haiyong Yang, and Shang Ma. "High-Speed Virtual Flight Testing Platform for Performance Evaluation of Pitch Maneuvers." Aerospace 10, no. 11 (2023): 962. http://dx.doi.org/10.3390/aerospace10110962.

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To research serious nonlinear coupling problems among aerodynamics, flight mechanics, and flight control during high maneuvers, a virtual flight testing platform has been developed for a large-scale, high-speed wind tunnel, based on the real physical environment, and it can significantly mitigate risks and reduce the costs of subsequent flight tests. The platform of virtual flight testing is composed of three-degrees-of-freedom model support, measuring devices for aerodynamic and motion parameters, a virtual flight control system, and a test model. It provides the ability to realistically simu
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Cai, Haohao, and Xiaomei Xu. "Lateral Stability Control of a Tractor-Semitrailer at High Speed." Machines 10, no. 8 (2022): 716. http://dx.doi.org/10.3390/machines10080716.

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To improve the high-speed lateral stability of the tractor-semitrailer, a lateral stability control strategy based on the additional yaw moment caused by differential braking is proposed and investigated based on the co-simulation environment. First of all, a five-degree-of-freedom (5-DOF) yaw-roll dynamic model of the tractor-semitrailer is established, and the model accuracy is verified. Secondly, the lateral stability control strategy of the tractor-semitrailer is proposed, two yaw moment controllers and the braking torque distributor are designed. Then, the effectiveness of the proposed co
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Rodriguez, Renato, Yan Wang, Joseph Ozanne, Dogan Sumer, Dimitar Filev, and Damoon Soudbakhsh. "Adaptive Takeoff Maneuver Optimization of a Sailing Boat for America’s Cup." Journal of Sailing Technology 7, no. 01 (2022): 88–103. http://dx.doi.org/10.5957/jst/2022.7.4.88.

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This paper presents the development of optimal takeoff maneuvers for an AC75 foiling sailboat competing in the oldest and most prestigious sailboat competition in the world, America’s Cup. The AC75 sailboat presents many challenges to developing these optimal maneuvers due to its nonlinear, high-dimensional, and highly unstable dynamics. During the takeoff maneuver, the boat starts in the water with low speed (displacement mode) and increases its speed until it reaches steady-state foiling (the hull stays out of the water). We optimized the time for the boat’s transitions from displacement mod
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Kitano, M., K. Watanabe, Y. Takaba, and K. Togo. "Lane-change maneuver of high speed tracked vehicles." Journal of Terramechanics 25, no. 2 (1988): 91–102. http://dx.doi.org/10.1016/0022-4898(88)90017-1.

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Hirano, Masahiro, Akihito Noda, Masatoshi Ishikawa, and Yuji Yamakawa. "Networked high-speed vision for evasive maneuver assist." ICT Express 3, no. 4 (2017): 178–82. http://dx.doi.org/10.1016/j.icte.2017.11.008.

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Quinn, Daniel, Daniel Kress, Eric Chang, Andrea Stein, Michal Wegrzynski, and David Lentink. "How lovebirds maneuver through lateral gusts with minimal visual information." Proceedings of the National Academy of Sciences 116, no. 30 (2019): 15033–41. http://dx.doi.org/10.1073/pnas.1903422116.

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Flying birds maneuver effectively through lateral gusts, even when gust speeds are as high as flight speeds. What information birds use to sense gusts and how they compensate is largely unknown. We found that lovebirds can maneuver through 45° lateral gusts similarly well in forest-, lake-, and cave-like visual environments. Despite being diurnal and raised in captivity, the birds fly to their goal perch with only a dim point light source as a beacon, showing that they do not need optic flow or a visual horizon to maneuver. To accomplish this feat, lovebirds primarily yaw their bodies into the
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HARA, Kiyoshi. "Safety of Collision Avoidance Maneuver under High Speed-Navigation." Journal of Japan Institute of Navigation 82 (1990): 69–75. http://dx.doi.org/10.9749/jin.82.69.

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Chen, Wenyu, Weimin Li, Lei Shao, and Tao Zhang. "Correction Strategy of Online Midcourse Guidance for High-Speed Gliding Target Interceptor." Applied Sciences 13, no. 11 (2023): 6661. http://dx.doi.org/10.3390/app13116661.

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During the interception of a high-speed gliding vehicle (HGV), the predicted intercept point (PIP) is updated many times, so the interceptor must continuously adjust its trajectory. In this paper, we propose an online guidance correction algorithm for the interceptor, which can effectively meet the position constraints and energy management of the guidance process. Firstly, we simplify the interceptor’s maneuvering problem to a two-body orbital transfer problem. The Lambert orbit transfer method is used to enable the interceptor to maneuver towards the target’s PIP. Secondly, by comparing the
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Yasukawa, Hironori, Noritaka Hirata, and Yoshiyuki Nakayama. "High-Speed Ship Maneuverability." Journal of Ship Research 60, no. 04 (2016): 239–58. http://dx.doi.org/10.5957/jsr.2016.60.4.239.

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In this paper, the effects of changes in hull attitude and the presence of stern append- ages such as rudders, shaft brackets, bossing, and propeller shafts on the maneuver- ability of a high-speed ship are investigated. The study is conducted for a ship operating within a Froude number range of 0.6–1.0. To determine the effect of attitude changes on the hydrodynamic derivatives during maneuvering, the hydrodynamic forces acting on the ship model with/without stern appendages are measured in three conditions: an even keel with the designed draft, and the same setup including hull rise or trim.
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Dissertations / Theses on the topic "High speed maneuver"

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Penco, Dario. "Contrôle véhicule autonome. Contrôle robuste et haute performance pour permettre les manœuvres à haute dynamique des véhicules autonomes." Electronic Thesis or Diss., université Paris-Saclay, 2022. http://www.theses.fr/2022UPASG039.

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Le travail abordé dans ces travaux de thèse se place dans le contexte de la conduite autonome. Plus particulièrement, l'objectif est le développement d'une loi de commande pour le suivi de trajectoire d'un véhicule autonome pour des manœuvres d'évitement d'obstacles à haute dynamique.Plusieurs modèles non-linéaires de dynamique du véhicule, capables de représenter son comportement dans des manœuvres à haute dynamique, sont proposés. Le but de la modélisation est d'obtenir un modèle pour la synthèse des correcteurs. L'ensemble de modèles proposés considère les dynamiques des vitesses longitudin
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Book chapters on the topic "High speed maneuver"

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Hui, Xiangyang, Fenghua Chi, Zheng Qi, Meng Wu, and Fei Li. "High-Speed Reentry Vehicle Trajectory Optimization and Guidance with Lateral Maneuver." In Lecture Notes in Electrical Engineering. Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-8155-7_346.

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Florence, Pete, John Carter, and Russ Tedrake. "Integrated Perception and Control at High Speed: Evaluating Collision Avoidance Maneuvers Without Maps." In Springer Proceedings in Advanced Robotics. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-43089-4_20.

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Maisser, P., and U. Jungnickel. "Stability of Controlled Motion of a Gymnast in High-Speed Mid Air Maneuvers." In IUTAM Symposium on Recent Developments in Non-linear Oscillations of Mechanical Systems. Springer Netherlands, 2000. http://dx.doi.org/10.1007/978-94-011-4150-5_13.

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Cushman, Stephen. "The Merit of Philip H. Sheridan’s Memoir Campaign." In The Generals' Civil War. University of North Carolina Press, 2021. http://dx.doi.org/10.5149/northcarolina/9781469666020.003.0006.

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Hoping to capitalize on the success of Grant’s memoir, Mark Twain approached Philip H. Sheridan to ask him to write his memoir as well. But by 1888, the Civil War memory market was becoming saturated with generals’ books, and Twain’s assistant at Charles L. Webster and Company warned that sales of Sheridan’s book would never equal those of Grant’s, despite Sheridan’s wide popularity at the time. Nevertheless, Sheridan wrote an excellent memoir in which he created a persona who was frank about his shortcomings, among them his tendency toward insubordination, and about his strengths, among them
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Zhang, Meiheng. "Research on Fast Extraction of Soccer Robot Movement Trajectories Based on Improved Low-Rank Trajectory Recovery." In Advances in Transdisciplinary Engineering. IOS Press, 2024. http://dx.doi.org/10.3233/atde240462.

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This paper presents a computer-assisted rapid trajectory extraction technique for soccer robots’ global vision system, focusing on Low-Rank Trajectory Recovery (LRTR). This system is crucial for providing robot posture data, enhancing decision-making, robot trajectories, and maneuver strategies. Given the competition rules demanding quick onsite vision system setup and adjustment, this method offers a speedy and accurate extracction process. It aims to refine trajectory tracking precision in high-level soccer matches, especially by processing varied noisy images in real scenarios. The study de
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Devarajan Venkat, Scott Daniel, Jones Daniel, et al. "Bimanual Haptic Workstation for Laparoscopic Surgery Simulation." In Studies in Health Technology and Informatics. IOS Press, 2001. https://doi.org/10.3233/978-1-60750-925-7-126.

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Realistic laparoscopic surgical simulators will require real-time graphic imaging and tactile feedback. Our research objective is to develop a cost-effective haptic workstation for the simulation of laparoscopic procedures for training and treatment planning. The physical station consists of a custom-built frame into which laparoscopic trocars and surgical tools may be attached/inserted and which are continuously adjustable to various positions and orientations to simulate multiple laparoscopic surgical approaches. Instruments inserted through the trocars are attached to end effectors of two h
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"Scott and Tabibi phase into the other by feeding it into the vicinity of the mixing/dispersing element. In this way, the phase being added is quickly dispersed into the continuous phase. Although it is widely accepted that the higher the shear rate produced by the mixer the smaller the droplets and, hence, the more stable the emulsion, there is a major prob-lem that must be avoided if good results are to be obtained with high-speed mixing equipment. Every effort should be made to avoid incorporating air into the mix. Air forms a third phase that could ruin emulsion stability in a number of ways. Air usu-ally reduces the viscosity. The addition steps should be organized such that the impel-ler of the mixture is always submerged deeply enough to avoid surface turbulence or splashing. The arrangement of the mixer angle and/or baffles should avoid vortexing. Another alternative is to perform all of the emulsion-making steps in a vacuum-pro-cessing vessel. An additional method is to premix the components at low speeds and shear rates and then subsequently execute the high-shear portion of the process with in-line equipment in the absence of air. In short, aeration should be avoided. Sometimes the direct approach is not the most effective one. When one phase is first added to another, the small amount of liquid being added forms the internal phase. If more of this liquid is added there comes a point where the continuous phase loses its ability to hold all of the internal phase and the emulsion inverts to the opposite type, e.g., from O/W to W/O. Since it has been found that this practice (phase inversion) can yield small droplet sizes, this method is widely used in batch processing. To ex-ecute this maneuver, one needs to begin mixing with only a small amount of liquid in a batch that will later increase to usually more than four times the starting volume. Therefore, the mixer has to extend well to the bottom of the vessel. One way to avoid this small volume of starting liquid is by using an in-line mixer in a recirculation loop attached to the main mixing vessel as illustrated in Fig. 5. The initial phase is recirculated through the in-line high mixer and the phase to be inverted is then carefully metered directly into the recirculation line. This avoids Fig. 5 In-line mixer in recirculation loop to kettle." In Pharmaceutical Dosage Forms. CRC Press, 1998. http://dx.doi.org/10.1201/9781420000955-37.

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Conference papers on the topic "High speed maneuver"

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Horn, Joseph, Adam Thorsen, and Angelina Conti. "Towards Handling Qualities Requirements for High-Speed Compound Rotorcraft." In Vertical Flight Society 73rd Annual Forum & Technology Display. The Vertical Flight Society, 2017. http://dx.doi.org/10.4050/f-0073-2017-12066.

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Handling qualities requirements for future high-speed rotorcraft are investigated. Two Mission Task Elements (MTEs) are developed and tested in piloted simulations of a notional winged compound rotorcraft with a full authority Non-linear Dynamic Inversion (NLDI) controller. The combat break turn maneuver was modified from a previously developed break turn MTE, and a formula for time-to-complete was derived to separate rotorcraft performance properties from the handling qualities. A decelerating approach MTE was modified from the current MTE in ADS-33F to use a Precision Approach Path Indicator
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A., Abhishek, and Rahul R. "Investigation of Tip-Vortex Modifications on Rotor Loads and Performance." In Vertical Flight Society 71st Annual Forum & Technology Display. The Vertical Flight Society, 2015. http://dx.doi.org/10.4050/f-0071-2015-10158.

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This paper studies the influence of tip vortex modification on the airloads and performance of the helicopter for high speed steady level flight and unsteady maneuver using a lifting-line based comprehensive analysis. The tip vortex modification is modeled inside the free wake model of the comprehensive analysis in three different ways: (1) the location of tip vortex release point is altered, keeping the strength constant, (2) strength of the tip vortex is diminished by certain factor while keeping the release location constant, and (3) both the release location and strength of the vortex are
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Chen, Yong, Sebastien Ghinet, Andrew Price, Viresh Wickramasinghe, and Anant Grewal. "Evaluation of Aircrew Whole-Body Vibration Exposure Levels on a Canadian CH-147F Chinook Helicopter." In Vertical Flight Society 72nd Annual Forum & Technology Display. The Vertical Flight Society, 2016. http://dx.doi.org/10.4050/f-0072-2016-11418.

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Flight testing has been performed on a Royal Canadian Air Force (RCAF) CH-147F Chinook helicopter to investigate aircrew whole-body vibration (WBV) exposure levels in accordance with ISO 2631-1 or MIL-STD-1472G standard. Results showed that the helicopter cabin vibration was dominated at the N/rev harmonics of the three-bladed tandem rotor speed. The aircrew WBV levels varied significantly depending on flight conditions and aircraft load configurations while the highest levels of WBV occurred at high speed level flight maneuver conditions. With reference to the guidelines in the standards, the
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Ventura Diaz, Patricia, Karl Edquist, and Seokkwan Yoon. "High-Fidelity Computational Modeling of Dragonfly Lander during Preparation for Powered Flight." In Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society, 2025. https://doi.org/10.4050/f-0081-2025-114.

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The Dragonfly relocatable lander was selected as NASA's New Frontiers mission in 2019 to explore the organic-rich surface of Titan, Saturn's largest moon. The coaxial quadrotor vehicle will fly to multiple geologic sites covering a distance of over 50 miles near the Titan equator. At each site, Dragonfly will sample materials, determine the surface composition, and investigate how far prebiotic chemistry has progressed on Titan. Upon arrival, the lander will enter the Titan atmosphere protected inside an aeroshell, which will descend and decelerate with parachutes. At an altitude of approximat
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Droandi, Giovanni, Monica Syal, and Geoffrey Bower. "Tiltwing Multi-Rotor Aerodynamic Modeling in Hover, Transition and Cruise Flight Conditions." In Vertical Flight Society 74th Annual Forum & Technology Display. The Vertical Flight Society, 2018. http://dx.doi.org/10.4050/f-0074-2018-12674.

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The paper discusses the aerodynamic modeling of a multi-rotor, tandem tiltwing aircraft called Vahana. Vahana is an all-electric, fully-autonomous aircraft being built by A3 by Airbus LLC. Vahana can take off and land vertically using eight fans, and can transition into cruise using fans and tilting wings. Vahana is designed to be able to trim at any speed during transition, even with the failure of any one of its eight motors. Aerodynamic modeling of Vahana is a challenging problem because of the interactions between multiple fans and wings during transition. In the present work, a medium-fid
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Ivler, Christina, and Ondrej Juhasz. "Evaluation of Control Allocation Techniques for a Medium Lift Tilt-Rotor." In Vertical Flight Society 71st Annual Forum & Technology Display. The Vertical Flight Society, 2015. http://dx.doi.org/10.4050/f-0071-2015-10169.

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In a traditional single main rotor helicopter, only 4 controls are available - lateral cyclic, longitudinal cyclic, main rotor collective pitch and tail rotor collective pitch. As such, redundancy is not available as all four controls are needed to maneuver the aircraft in the four control axes - pitch, roll, yaw and heave. In contrast, high speed rotorcraft configurations (such as tilt-rotors and compound helicopters) have multiple redundant control effectors. The strategy for applying these control effectors, and in which proportion, is called 'control allocation'. This paper provides an eva
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Scaramal, Mariano, Jacob Enciu, and Joseph Horn. "Active Stabilization of Slung Loads in High Speed Flight Using Cable Angle Feedback." In Vertical Flight Society 74th Annual Forum & Technology Display. The Vertical Flight Society, 2018. http://dx.doi.org/10.4050/f-0074-2018-12842.

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This paper addresses the problem of active stabilization of slung loads at high speed flight. To demonstrate the method, simulations of a utility helicopter with a dynamic inversion controller (as its automatic flight control system) and a CONEX cargo container were used. An airspeed scheduled controller utilizing cable angle feedback was designed for the nonlinear coupled system by the classic root locus technique. Nonlinear simulations of straight and level flight at different airspeeds were used to validate the controller performance in stabilizing the load pendulum motions. Controller perf
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Voskuijl, Mark, and Mario Verhagen. "Helicopter Main Rotor Hub Load Alleviation Using a Variable Incidence Horizontal Stabilizer." In Vertical Flight Society 72nd Annual Forum & Technology Display. The Vertical Flight Society, 2016. http://dx.doi.org/10.4050/f-0072-2016-11448.

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A new technique to reduce the main rotor hub forces and moments at high speed maneuvers is proposed. The main working principle is a mechanical gearing ratio that distributes pitch commands from the (auto)pilot over main rotor cyclic pitch and the horizontal stabilizer incidence angle. The optimal gearing ratio is determined by the weighted pseudo inverse method. The system is analyzed with a nonlinear simulation model of the UH-60A Black Hawk helicopter. Results demonstrate that the main rotor shaft bending moment can be reduced by more than 50% for high speed pitch maneuvers whilst maintaini
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Kunchakuri, Naveen. "MATLAB-Based Simulation of Generative AI-Based Autonomous Vehicle Control for High-Speed Driving and Emergency Maneuvers." In 2025 First International Conference on Advances in Computer Science, Electrical, Electronics, and Communication Technologies (CE2CT). IEEE, 2025. https://doi.org/10.1109/ce2ct64011.2025.10939159.

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Brewer, Roy, Frank Conway, and Ray Mulato. "Development and Evaluation of New High-Speed ADS-33 Mission Task Elements using a Tiltrotor Platform." In Vertical Flight Society 73rd Annual Forum & Technology Display. The Vertical Flight Society, 2017. http://dx.doi.org/10.4050/f-0073-2017-12067.

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The Boeing Company has developed and evaluated several new High Speed Mission Task Elements (MTEs) as part of the National Rotorcraft Technology Center (NRTC) program "Handling Qualities Requirements for Future Configurations and Missions". One of the main goals of this program, which is a collaboration between industry, academia and the U.S. Government, is to update the current Aeronautical Design Standard Performance Specification ADS-33E-PRF to provide the new MTEs that would be required to support Future Vertical Lift (FVL) requirements. Boeing's contribution to the program includes the fo
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Reports on the topic "High speed maneuver"

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Buck, Nicole L., Barry A. Coutermarsh, and Sally A. Shoop. Loose-Surface Tire-Terrain Interaction During High-Speed Maneuvers. Defense Technical Information Center, 2010. http://dx.doi.org/10.21236/ada533233.

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Volunteer Kinematics and Reaction in Lateral Emergency Maneuver Tests. SAE International, 2013. http://dx.doi.org/10.4271/2013-22-0013.

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It is important to understand human kinematics and muscle activation patterns in emergency maneuvers for the design of safety systems and for the further development of human models. The objective of this study was to quantify kinematic behavior and muscle activation in simulated steering tests in several realistic conditions. In total 108 tests were performed with 10 volunteers undergoing purely lateral maneuvers at 5 m/s2 deceleration or simulated lane change maneuvers at 5 m/s2 peak acceleration and peak yaw velocity of 25 °/s. Test subjects were seated on a rigid seat and restrained by a 4
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