Academic literature on the topic 'Gyroscopic systems'

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Journal articles on the topic "Gyroscopic systems"

1

Kudelin, Igor, Srikanth Sugavanam, and Maria Chernysheva. "Rotation Active Sensors Based on Ultrafast Fibre Lasers." Sensors 21, no. 10 (2021): 3530. http://dx.doi.org/10.3390/s21103530.

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Gyroscopes merit an undeniable role in inertial navigation systems, geodesy and seismology. By employing the optical Sagnac effect, ring laser gyroscopes provide exceptionally accurate measurements of even ultraslow angular velocity with a resolution up to 10−11 rad/s. With the recent advancement of ultrafast fibre lasers and, particularly, enabling effective bidirectional generation, their applications have been expanded to the areas of dual-comb spectroscopy and gyroscopy. Exceptional compactness, maintenance-free operation and rather low cost make ultrafast fibre lasers attractive for sensing applications. Remarkably, laser gyroscope operation in the ultrashort pulse generation regime presents a promising approach for eliminating sensing limitations caused by the synchronisation of counter-propagating channels, the most critical of which is frequency lock-in. In this work, we overview the fundamentals of gyroscopic sensing and ultrafast fibre lasers to bridge the gap between tools development and their real-world applications. This article provides a historical outline, highlights the most recent advancements and discusses perspectives for the expanding field of ultrafast fibre laser gyroscopes. We acknowledge the bottlenecks and deficiencies of the presented ultrafast laser gyroscope concepts due to intrinsic physical effects or currently available measurement methodology. Finally, the current work outlines solutions for further ultrafast laser technology development to translate to future commercial gyroscopes.
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2

Ünker, F., and O. Çuvalcı. "Optimum Tuning of a Gyroscopic Vibration Absorber Using Coupled Gyroscopes for Vibration Control of a Vertical Cantilever Beam." Shock and Vibration 2016 (2016): 1–10. http://dx.doi.org/10.1155/2016/1496727.

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This paper deals with the investigation of optimum values of the stiffness and damping which connect two gyroscopic systems formed by two rotors mounted in gimbal assuming negligible masses for the spring, damper, and gimbal support. These coupled gyroscopes use two gyroscopic flywheels, spinning in opposing directions to have reverse precessions to eliminate the forces due to the torque existing in the torsional spring and the damper between gyroscopes. The system is mounted on a vertical cantilever with the purpose of studying the horizontal and vertical vibrations. The equation of motion of the compound system (gyro-beam system) is introduced and solved to find the response measured on the primary system. This is fundamental to design, in some way, the dynamic absorber or neutralizer. On the other hand, the effect of the angular velocities of the gyroscopes are studied, and it is shown that the angular velocity (spin velocity) of a gyroscope has a significant effect on the behavior of the dynamic motion. Correctness of the analytical results is verified by numerical simulations. The comparison with the results from the derivation of the corresponding frequency equations shows that the optimized stiffness and damping values are very accurate.
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3

KHASMINSKII, R., and G. N. MILSTEIN. "STABILITY OF GYROSCOPIC SYSTEMS UNDER SMALL RANDOM EXCITATIONS." Stochastics and Dynamics 04, no. 01 (2004): 107–33. http://dx.doi.org/10.1142/s0219493704000924.

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Gyroscopic systems with two degrees of freedom under small random perturbations are investigated by use of the stochastic averaging principle. It is proved that the principal term of the Lyapunov exponent for the original system coincides with the Lyapunov exponent for the averaged system. An explicit formula for the averaged Lyapunov exponent is derived. The averaged moment Lyapunov exponent is also considered. An example is given in which an unstable gyroscopical system is stabilized by noise of the Stratonovich type.
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4

Hryniv, R., and P. Lancaster. "Stabilization of Gyroscopic Systems." ZAMM 81, no. 10 (2001): 675–81. http://dx.doi.org/10.1002/1521-4001(200110)81:10<675::aid-zamm675>3.0.co;2-r.

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5

Kuseyri, Sina. "Constrained H∞ control of gyroscopic ship stabilization systems." Proceedings of the Institution of Mechanical Engineers, Part M: Journal of Engineering for the Maritime Environment 234, no. 3 (2020): 634–41. http://dx.doi.org/10.1177/1475090220903217.

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We suggest a constrained [Formula: see text] control scheme for gyroscopic marine vehicle stabilization systems with output and control constraints. The [Formula: see text] performance is used to measure the roll angle reduction of the vessel relative to wave disturbances in regular beam seas. Time-domain constraints, representing requirements for precession angle of gyroscopes and for actuator saturation, are captured using the concept of reachable sets and state-space ellipsoids. A state feedback solution to the constrained [Formula: see text] stabilization control problem is proposed in the framework of linear matrix inequality optimization and multiobjective control. This approach can potentially achieve the best possible vessel comfort with respect to roll motion by allowing constrained variables free as long as they remain within given bounds. Analysis and simulation results for roll dynamics of the vessel coupled with the gyroscopic actuator control system show possible improvements on roll motion stabilization while respecting time-domain hard constraints.
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6

Yang, B. "Eigenvalue Inclusion Principles for Discrete Gyroscopic Systems." Journal of Applied Mechanics 59, no. 2S (1992): S278—S283. http://dx.doi.org/10.1115/1.2899501.

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In his famous treatise The Theory of Sound, Rayleigh enunciated an eigenvalue inclusion principle for modified discrete nongyroscopic systems. According to this principle, the natural frequencies of a nongyroscopic system without and with modification are alternatively located along the positive real axis. Although vibration and dynamics of discrete gyroscopic systems have been extensively studied, the problem of inclusion principles for discrete gyroscopic systems has not been addressed. This paper presents several eigenvalue inclusion principles for a class of discrete gyroscopic systems. A transfer function formulation is proposed to describe modified gyroscopic systems. Six types of modifications and their effects on the system natural frequencies are studied. It is shown that the transfer function formulation provides a systematic and convenient way to handle modification problems for discrete gyroscopic systems.
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7

Barkwell, Lawrence, and Peter Lancaster. "Overdamped and Gyroscopic Vibrating Systems." Journal of Applied Mechanics 59, no. 1 (1992): 176–81. http://dx.doi.org/10.1115/1.2899425.

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Some linear vibrating systems give rise to differential equations of the form Ix¨(t) + Bx˙(t) + Cx(t) = 0, where B and C are square matrices. Stability criteria involving only the matrix coefficients I, B, C, and a single parameter are obtained for some special cases. Thus, if B* = B&gt; 0, C* = C&gt;0 and B&gt;kI + k−1C, then the system will be overdamped (and hence stable). Gyroscopic systems also have the above form where B is real and skew symmetric. The case where C&gt;0 is well understood and for the case −C&gt;0 we show the condition Babs&gt;kI−k−1C for some k&gt;0 will ensure stability. In fact, this condition can be generalized to systems with B* = B, C&gt;0.
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8

Ariaratnam, S. T., and N. Sri Namachchivaya. "Periodically Perturbed Linear Gyroscopic Systems*." Journal of Structural Mechanics 14, no. 2 (1986): 127–51. http://dx.doi.org/10.1080/03601218608907513.

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9

Ariaratnam, S. T., and N. Sri Namachchivaya. "Periodically Perturbed Nonlinear Gyroscopic Systems*." Journal of Structural Mechanics 14, no. 2 (1986): 153–75. http://dx.doi.org/10.1080/03601218608907514.

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10

Datta, B. N., Y. M. Ram, and D. R. Sarkissian. "Spectrum Modification for Gyroscopic Systems." ZAMM 82, no. 3 (2002): 191–200. http://dx.doi.org/10.1002/1521-4001(200203)82:3<191::aid-zamm191>3.0.co;2-l.

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