Thematische Bibliographien / Yaw velocity

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Auswahl der wissenschaftlichen Literatur zum Thema „Yaw velocity“

Autor: Grafiati

Veröffentlicht am 4. Juni 2021

Zuletzt aktualisiert am 10. Februar 2022

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Zeitschriftenartikel zum Thema "Yaw velocity"

Wang, Hong Wei, Chen Jie Qi, Qiu Xin Wu, Qi Mu Surong und Zhen Hua Xing. „Signal Decomposition for Three-Axis Gyroscope“. Advanced Materials Research 346 (September 2011): 521–26. http://dx.doi.org/10.4028/www.scientific.net/amr.346.521.

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Study Algorithm of roll, pitch and yaw angular velocity for three-axis gyroscope. the gyro have only one sensitive quality, can sensitize the three axial angular velocity of the rotating carrier at the same time. in the case of gyro’s spin angular velocity presence and pitch or yaw angular velocity worked, gyro output signal contain spin, pitch and yaw angular velocity. Through Uniaxial Gravity Accelerometer’s application, the roll, pitch and yaw angular velocity for three-axis gyroscope can be demodulated.

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John, J., und T. Schobeiri. „A Simple and Accurate Method of Calibrating X-Probes“. Journal of Fluids Engineering 115, Nr. 1 (01.03.1993): 148–52. http://dx.doi.org/10.1115/1.2910098.

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This paper presents an improved method of calibrating hot-film X-probes in incompressible flow. The yaw response of a hot-film X-probe was investigated for different velocities and found to be strongly velocity dependent at low velocities. A simple relation was developed to correct for the variation of yaw response at low velocities. The method using the yaw correction is compared with the single-velocity yaw calibration method. The correction to the yaw response considerably improves accuracy at low velocities.

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Sun, Tao, Hao Guo, Jian-yong Cao, Ling-jiang Chai und Yue-dong Sun. „Study on Integrated Control of Active Front Steering and Direct Yaw Moment Based on Vehicle Lateral Velocity Estimation“. Mathematical Problems in Engineering 2013 (2013): 1–8. http://dx.doi.org/10.1155/2013/275269.

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Considering the vehicle lateral velocity is difficult to be measured at integration of chassis control in configuration of production vehicle, this study presents the vehicle lateral velocity estimation based on the extended Kalman filtering with the standard sensor information. The fuzzy control algorithm is proposed to integrate direct yaw moment control and active front steering with lateral velocity estimation. The integration controller produces direct yaw moment and front wheel angle compensation to control yaw rate and sideslip angle, which makes the actual vehicle yaw rate and sideslip angle follow desirable yaw rate and desirable sideslip angle. The simulation results show vehicle handling and stability are enhanced under different driving cycles by the proposed algorithm.

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Walker, Mark F., und David S. Zee. „Cerebellar Disease Alters the Axis of the High-Acceleration Vestibuloocular Reflex“. Journal of Neurophysiology 94, Nr. 5 (November 2005): 3417–29. http://dx.doi.org/10.1152/jn.00375.2005.

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L. W. Schultheis and D. A. Robinson showed that the axis of the rotational vestibuloocular reflex (RVOR) cannot be altered by visual-vestibular mismatch (“cross-axis adaptation”) when the vestibulocerebellum is lesioned. This suggests that the cerebellum may calibrate the axis of eye velocity of the RVOR under natural conditions. Thus we asked whether patients with cerebellar disease have alterations in the RVOR axis and, if so, what might be the mechanism. We used three-axis scleral coils to record head and eye movements during yaw, pitch, and roll head impulses in 18 patients with cerebellar disease and in a comparison group of eight subjects without neurologic disease. We found distinct shifts of the eye-velocity axis in patients. The characteristic finding was a disconjugate upward eye velocity during yaw. Measured at 70 ms after the onset of head rotation, the median upward gaze velocity was 15% of yaw head velocity for patients and <1% for normal subjects ( P < 0.001). Upward eye velocity was greater in the contralateral (abducting) eye during yaw and in the ipsilateral eye during roll. Patients had a higher gain (eye speed/head speed) for downward than for upward pitch (median ratio of downward to upward gain: 1.3). In patients, upward gaze velocities during both yaw and roll correlated with the difference in anterior (AC) and posterior canal excitations, scaled by the respective pitch gains. Our findings support the hypothesis that upward eye velocity during yaw results from AC excitation, which must normally be suppressed by the intact cerebellum.

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Emirler, Mümin Tolga, Kerim Kahraman, Mutlu Şentürk, Bilin Aksun Güvenç, Levent Güvenç und Barış Efendioğlu. „Vehicle Yaw Rate Estimation Using a Virtual Sensor“. International Journal of Vehicular Technology 2013 (24.04.2013): 1–13. http://dx.doi.org/10.1155/2013/582691.

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Road vehicle yaw stability control systems like electronic stability program (ESP) are important active safety systems used for maintaining lateral stability of the vehicle. Vehicle yaw rate is the key parameter that needs to be known by a yaw stability control system. In this paper, yaw rate is estimated using a virtual sensor which contains kinematic relations and a velocity-scheduled Kalman filter. Kinematic estimation is carried out using wheel speeds, dynamic tire radius, and front wheel steering angle. In addition, a velocity-scheduled Kalman filter utilizing the linearized single-track model of the road vehicle is used in the dynamic estimation part of the virtual sensor. The designed virtual sensor is successfully tested offline using a validated, high degrees of freedom, and high fidelity vehicle model and using hardware-in-the-loop simulations. Moreover, actual road testing is carried out and the estimated yaw rate from the virtual sensor is compared with the actual yaw rate obtained from the commercial yaw rate sensor to demonstrate the effectiveness of the virtual yaw rate sensor in practical use.

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Schottler, Jannik, Jan Bartl, Franz Mühle, Lars Sætran, Joachim Peinke und Michael Hölling. „Wind tunnel experiments on wind turbine wakes in yaw: redefining the wake width“. Wind Energy Science 3, Nr. 1 (16.05.2018): 257–73. http://dx.doi.org/10.5194/wes-3-257-2018.

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Abstract. This paper presents an investigation of wakes behind model wind turbines, including cases of yaw misalignment. Two different turbines were used and their wakes are compared, isolating effects of boundary conditions and turbine specifications. Laser Doppler anemometry was used to scan full planes of wakes normal to the main flow direction, six rotor diameters downstream of the respective turbine. The wakes of both turbines are compared in terms of the time-averaged main flow component, the turbulent kinetic energy and the distribution of velocity increments. The shape of the velocity increments' distributions is quantified by the shape parameter λ2. The results show that areas of strongly heavy-tailed distributed velocity increments surround the velocity deficits in all cases examined. Thus, a wake is significantly wider when two-point statistics are included as opposed to a description limited to one-point quantities. As non-Gaussian distributions of velocity increments affect loads of downstream rotors, our findings impact the application of active wake steering through yaw misalignment as well as wind farm layout optimizations and should therefore be considered in future wake studies, wind farm layout and farm control approaches. Further, the velocity deficits behind both turbines are deformed to a kidney-like curled shape during yaw misalignment, for which parameterization methods are introduced. Moreover, the lateral wake deflection during yaw misalignment is investigated.

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May, M. L., und R. R. Hoy. „Ultrasound-induced yaw movements in the flying Australian field cricket (Teleogryllus oceanicus)“. Journal of Experimental Biology 149, Nr. 1 (01.03.1990): 177–89. http://dx.doi.org/10.1242/jeb.149.1.177.

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An ultrasonic stimulus induced negative phonotactic steering in the yaw axis of tethered, flying Australian field crickets. The forewings, hindwings and twisting of the thorax generated the forces which induced the yaw turn. However, abdominal ruddering did not contribute to yaw turns. Each aspect of the yaw steering response depended upon the stimulus intensity. At higher ultrasonic intensities, the magnitude and average angular velocity increased while the latency of the yaw turn decreased. Each of these factors varied in a graded manner, revealing that this behavior is more complex than a simple reflex.

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Killian, J. Eric, und James F. Baker. „Horizontal Vestibuloocular Reflex (VOR) Head Velocity Estimation in Purkinje Cell Degeneration (pcd/pcd) Mutant Mice“. Journal of Neurophysiology 87, Nr. 2 (01.02.2002): 1159–64. http://dx.doi.org/10.1152/jn.00219.2001.

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The horizontal vestibuloocular reflex (VOR) of Purkinje cell degeneration ( pcd/pcd) mutant mice, which lack a functional cerebellar cortex, was compared in darkness to that of wild-type animals during constant velocity yaw rotations about an earth-horizontal axis and during sinusoidal yaw rotations about an earth-vertical axis. Both wild-type and pcd/pcd mice showed a compensatory average VOR eye velocity, or bias, during constant velocity horizontal axis rotations, evidence of central neural processing of otolith afferent signals to create a signal proportional to head angular velocity. Eye velocity bias was greater in pcd/pcd mice than in wild-type mice at a low rotational velocity (32°/s), but less at higher velocities (128 and 200°/s). Lesion of the medial nodulus severely attenuated eye velocity bias in two wild-type mice, without attenuating VOR during sinusoidal vertical axis yaw rotations at 0.2 Hz. These results show that while head velocity estimation in mice, as in primates, depends on the cerebellum, pcd/pcd mutant mice develop velocity estimation without a functional cerebellar cortex. We conclude that neural circuits that exclude cerebellar cortex are capable of the signal processing necessary for head angular velocity estimation, but that these circuits are insufficient for normal estimation at high velocities.

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Lafortune, S. H., D. J. Ireland und R. M. Jell. „Effect of active head movements about the pitch, roll, and yaw axes on human optokinetic afternystagmus“. Canadian Journal of Physiology and Pharmacology 66, Nr. 6 (01.06.1988): 689–96. http://dx.doi.org/10.1139/y88-110.

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Effects of active head movements about the pitch, roll, or yaw axes on horizontal optokinetic afternystagmas (OKAN) were examined in 16 subjects to test the hypothesis that otolith organ mediated activity induced by a change in head position can couple to the horizontal velocity storage in humans. Active head movements about the pitch axis, forwards or backwards, produced significant OKAN suppression. Pitch forward head movements exerted the strongest effect. Active head movements about the roll axis towards the right also produced OKAN suppression but only if the tilted position was sustained. No suppression was observed following sustained yaw. However, an unsustained yaw left movement after rightward drum rotation significantly enhanced OKAN. Sustained head movement trials did not significantly alter subsequent control trials. In contrast, unsustained movements about the pitch axis, which involve more complex interactions, exerted long-term effects on subsequent control trials. We conclude that otolith organ mediated activity arising from pitch or roll head movements couples to the horizontal velocity storage in humans, thereby suppressing ongoing OKAN. Activity arising from the horizontal canals during an unsustained yaw movement (observed mainly with yaw left), following drum rotation in a direction contralateral to the movement, may also couple to the velocity storage, resulting in increased activity instead of suppression.

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Zhao, Ming Hui, Lian Dong Wang, Lei Ma und Hui Hou. „Control Methods of Active Front Wheel Steering for 4WD Electric Vehicle“. Applied Mechanics and Materials 97-98 (September 2011): 735–40. http://dx.doi.org/10.4028/www.scientific.net/amm.97-98.735.

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Based on two freedom degrees of vehicle model, control method which takes yaw rate and sideslip angle as system state, and front wheel corner and direct yaw moment as control input is put forward. Considering uncertainty of velocity and direct yaw moment, feedforward-feedback controllers are designed. Four wheel drive force are allocated by using feedforward compensation and yaw moment which is formed by driving force difference value. It makes yaw rate and sideslip well of tracking the desirable model when the vehicle drive steering. Finally, vehicle handling stability is studied on conditions of step input and sine input by simulation.

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Dissertationen zum Thema "Yaw velocity"

Jegede, Olaseinde. „Dual-axis fluidic thrust vectoring of high-aspect ratio supersonic jets“. Thesis, University of Manchester, 2016. https://www.research.manchester.ac.uk/portal/en/theses/dualaxis-fluidic-thrust-vectoring-of-highaspect-ratio-supersonic-jets(6d6a5867-8281-4dfd-ac45-105ff4e73e39).html.

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A dual-axis fluidic thrust vectoring (FTV) system is proposed where the supersonic propulsive jet of an aircraft is exhausted over a scarfed (swept), curved surface to produce flight control moments in both the pitch and yaw axes. This work contributes towards practical dual-axis FTV through expansion of fundamental curved-wall jet (CWJ) understanding, development of the novel Superimposed Characteristics technique for supersonic nozzle design, and performance evaluation of an experimental scarfed curved wall FTV configuration. Previous work has suggested that the use of a sheared exhaust velocity profile improves the attachment of supersonic jets to curved surfaces; however, evidence to support this is limited. To address this, an inviscid numerical CWJ model was developed using the two-dimensional method of characteristics. A major outcome is improved understanding of the effect of exhaust velocity profile on CWJ wave structure and subsequent jet attachment. A sheared velocity exhaust is shown to generate a wave structure that diminishes adverse streamwise pressure gradients within a supersonic curved-wall jet. This reduces the likelihood of boundary layer separation and as a result, a sheared exhaust velocity CWJ is expected to be less readily separated compared to other exhaust velocity profiles. A novel method termed Superimposed Characteristics was developed for the low-order design of supersonic nozzles with rectangular exits. The technique is capable of generating 3D nozzle geometries based on independent exit plane orientation and exhaust velocity distribution requirements. The Superimposed Characteristics method was used to design scarfed rectangular exit nozzles with sheared velocity exhaust profiles. These nozzles were then evaluated using finite volume computational methods and experimental methods. From the analysis, the Superimposed Characteristics method is shown to be valid for preliminary nozzle design. Experimental methods were used to study the on- and off-design attachment qualities of uniform and sheared velocity exhaust jets for a FTV configuration with an external curved wall termination angle of 90 degrees and scarf angle of 30 degrees. Experiments at the on-design nozzle pressure ratio (NPR) of 3.3 demonstrated pitch and yaw jet deflection angles of 78 degrees and 23 degrees respectively for the uniform exhaust velocity CWJ. The sheared exhaust velocity CWJ achieved lower pitch and yaw deflection angles of 34 degrees and 14 degrees respectively at the same on-design NPR. The lower jet deflection angles observed for sheared exhaust velocity jets is inconsistent with the CWJ model prediction of reduced adverse streamwise pressure gradients; however, there was insufficient experimental instrumentation to identify the cause. In the off-design experiments, the uniform exhaust velocity CWJ was observed to detach at an NPR of 3.6, whilst the sheared exhaust velocity CWJ remained attached at NPRs in excess of 4. The capability of sheared exhaust velocity CWJs to remain attached at higher NPRs is consistent with the analytical theory and the CWJ model predictions. An actuation study was carried out to achieve controlled jet detachment using secondary blowing injected normal to the curved wall. Full separation of the wall jets was achieved downstream of the injection point. This provided vectoring angles of more than 20 degrees in pitch and 10 degrees in yaw, exceeding expected vectoring requirements for practical aircraft control. At the on-design NPR, the uniform and sheared exhaust velocity jets required secondary blowing mass flow rates of 2.1% and 3.8% of the primary mass flow respectively to achieve full separation.

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Lojková, Lea. „Experimentální metodologie měřicího řetězce“. Master's thesis, Vysoké učení technické v Brně. Fakulta elektrotechniky a komunikačních technologií, 2011. http://www.nusl.cz/ntk/nusl-219052.

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This work is focused on the development of a thorough study about ISO standards focused on the vehicle dynamics, standardized tests of vehicle dynamics and measured variables that allow us to describe and model the behaviour of riding vehicles properly. In the Appendix A of the thesis, there is a list of all known ISO standards dealing with given topic. The standard ISO 15037-1 Road vehicles – Vehicle dynamics test methods, Part 1: General conditions for passenger cars is described in detail, including the forms for test reports and the Appendix C and D. In the thesis, there is also described a model of minimal needed measuring system that is still in good accordance with the standard ISO 15037-1 and fulfills all its requirements. Detailed description of all used sensors that are used to measure required variables is given, as well as a short description of all sensors that are used for measurement of other variables. After that, measurement abilities of the instrumentation of measuring system RIO used in ÚADI FSI Brno is compared and confronted with requirements given by the standard, to see, if all given criteria are properly fulfilled. Because of the fact that standard-given criteria are quite mild, while the equipment of the faculty is high-level technology, mostly made directly for measuring of dynamic parameters of the vehicles, including racing vehicles, the system is in full accordance with the standard ISO 15037-1.

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Yao, Wei [Verfasser]. „Extraction and velocity estimation of vehicles in urban areas from airborne laserscanning data / Wei Yao“. 2010. http://d-nb.info/1010916270/34.

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Bücher zum Thema "Yaw velocity"

Effects of yaw and pitch motion on model attitude measurements. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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S, Tripp John, Finley Tom D und Langley Research Center, Hrsg. Effects of yaw and pitch motion on model attitude measurements. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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Center, Lewis Research, und United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., Hrsg. Rayleigh Scattering Diagnositics Workshop. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

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Buchteile zum Thema "Yaw velocity"

Ackermann, Juergen. „Velocity-Independent Yaw Eigenvalues of Four-Wheel Steering Automobiles“. In Robustness of Dynamic Systems with Parameter Uncertainties, 291–302. Basel: Birkhäuser Basel, 1992. http://dx.doi.org/10.1007/978-3-0348-7268-3_29.

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Lucet, Eric, Christophe Grand und Philippe Bidaud. „Sliding-Mode Velocity and Yaw Control of a 4WD Skid-Steering Mobile Robot“. In Advances in Intelligent and Soft Computing, 247–58. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-16259-6_19.

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„AK FfGgmI1,294 0,718 0,241 0,662 0,419 II 0,801 0,754 0,264 0,774 0,369 III-1 0,640 0,784 0,215 0,885 0,282 III-2 0,659 0,807 0,165 0,996 0,223 IV 0,876 0,823 0,127 1,108 0,205 V 1,503 0,833 0,151 1,219 0,089 Ak F F0 f G Go 9m50,25 194 0,72 0,69 48 0,59 0,40 4 1,19 354 0,67 0,60 42 0,74 0,28 3 0,82 198 0,74 0,09 12 1,11 0,22 2 0,94 168 0,76 0,08 12 1,28 0,11 Table 2. Coefficients of diffusivity dependent on stability classes after Klug and Turner; m stands for the exponent in the power law of wind velocity. However, we must keep in mind the limitations of this approach, especially the transfer of consistent sets of dispersion parameters to the propagation of air pollution in the vicinity of a source. The Gaussian plume formula should be used only for those downwind distances for which the empirical diffusion coefficients have been determined by standard diffusion experiments. Because we are interested in emissions near ground level and immissions nearby the source, we use those diffusion parameters which are based on the classification of Klug /12/ and Turner /13/. The parameters are expressible as power functions, Oy(x) = F xf and az(x) = G x9 after Klug (3.6a,b), tfy(x) = (F + Fx)f and az(x) = (GQ + Gx)9 after Turner (3.7a,b). The parameter classification after Klug is determined by six stability classes (with the German abbreviation AK for Ausbreitungsklasse), reaching from extreme stable (AK I) to extreme labile TAK V). In tRe Turner stability scheme AK 5 denotes extreme stable, AK 2 extreme labile, see table 2. An estimate of the stability can be made from synoptical observa tions of solar radiation, cloud cover and wind velocity /14/. With the parameters after Klug equation (3.4) becomes C(x,y,z) = ax"(f+9^exp(-bx"2f) [exp(-d0x"2g)+exp(-d1x"2g)] (3.8), wherein - - C0V k ya w (z-H)2 ^ (z+H) a ' TrTOFE • b ■ ■JT • do = -Z IP '- • d1 = ~75*~“. In Odour Prevention and Control of Organic Sludge and Livestock Farming, 120. CRC Press, 1986. http://dx.doi.org/10.1201/9781482286311-43.

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Konferenzberichte zum Thema "Yaw velocity"

Seifert, Sara J., Robert J. Dahlstrom, John P. Condon und Daniel S. Hedin. „Yaw rate and linear velocity stabilized manual wheelchair“. In 2013 35th Annual International Conference of the IEEE Engineering in Medicine and Biology Society (EMBC). IEEE, 2013. http://dx.doi.org/10.1109/embc.2013.6609641.

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Rajesh, Sreeja, Derek Abbott und David C. O'Carroll. „A 16 pixel yaw sensor for velocity estimation“. In Microelectronics, MEMS, and Nanotechnology, herausgegeben von Dan V. Nicolau. SPIE, 2005. http://dx.doi.org/10.1117/12.639260.

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Jun, Wang, und Shengbing Yang. „Adaptive Yaw Angular Velocity Control of Electric Power Steering“. In SAE 2011 World Congress & Exhibition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2011. http://dx.doi.org/10.4271/2011-01-0759.

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Qin, Xuemei, Yehai Lin und Baoshan Shi. „Electrohydraulic servo control of vehicle yaw rate angular velocity“. In Mechanical Engineering and Information Technology (EMEIT). IEEE, 2011. http://dx.doi.org/10.1109/emeit.2011.6023494.

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Cherouat, H., M. Braci und S. Diop. „Vehicle velocity, side slip angles and yaw rate estimation“. In Proceedings of the IEEE International Symposium on Industrial Electronics. IEEE, 2005. http://dx.doi.org/10.1109/isie.2005.1528935.

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Rose, Nathan A., Neal Carter und Gray Beauchamp. „Post-Impact Dynamics for Vehicles with a High Yaw Velocity“. In SAE 2016 World Congress and Exhibition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2016. http://dx.doi.org/10.4271/2016-01-1470.

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Gustafsson, Fredrik, Stefan Ahlqvist, Urban Forssell und Niclas Persson. „Sensor Fusion for Accurate Computation of Yaw Rate and Absolute Velocity“. In SAE 2001 World Congress. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2001. http://dx.doi.org/10.4271/2001-01-1064.

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Karaman, S., S. Oncu, L. Guvenc, S. S. Ersolmaz, E. Cetin und A. Kanbolat. „Robust Velocity Scheduled Yaw Stability Control of a Light Commercial Vehicle“. In Proceedings of IV2006. IEEE Intelligent Vehicles Symposium. IEEE, 2006. http://dx.doi.org/10.1109/ivs.2006.1689678.

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COURTNEY, ELYA, ROY COUVILLION, AMY COURTNEY und MICHAEL COURTNEY. „Effects of Sound Suppressors on Muzzle Velocity, Bullet Yaw and Drag“. In 30th International Symposium on Ballistics. Lancaster, PA: DEStech Publications, Inc., 2017. http://dx.doi.org/10.12783/ballistics2017/16879.

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Peterson, Dale L., und Mont Hubbard. „Yaw Rate and Velocity Tracking Control of a Hands-Free Bicycle“. In ASME 2008 International Mechanical Engineering Congress and Exposition. ASMEDC, 2008. http://dx.doi.org/10.1115/imece2008-68948.

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The control of a bicycle has been well studied when a steer torque is used as the control input. Less has been done to investigate the control of a hands free bicycle through the rider’s lean relative to the bicycle frame. In this work, we extend a verified benchmark bicycle model to include a rider with the ability to lean in and out of the plane of the bicycle frame. A multi-input multi-output LQR state feedback controller is designed with the control objective being the tracking of a reference yaw rate and rear wheel angular velocity through the use of rider lean torque and rear wheel (pedaling) torque. The LQR controller is tested on the nonlinear model and numerical simulation results are presented. Conclusions regarding the required lean angle of the rider relative to the bicycle frame necessary to execute a steady turn are made, as well as observations of the effects of right half plane zeros in the transfer function from rider lean torque to yaw rate.

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Berichte der Organisationen zum Thema "Yaw velocity"

Pennekamp, Richard A. A Large-Caliber, High-Velocity Yaw Inducer. Fort Belvoir, VA: Defense Technical Information Center, November 1989. http://dx.doi.org/10.21236/ada216846.

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