This paper considers the dependence of the rotor tuning condition of a rotor-vibratory gyroscope on the elastic properties of the spring element which has, in particular, additional angular deflection along an axis perpendicular to the output axis of gyroscope. As a consequence of this dependence, the limitations to the performance of the rotor tuning condition are examined and a mathematical equation describing the rotor tuning error, dependent on variations in the gyroscope parameters, is obtained. Analysis of the equation of rotor tuning error allows us to formulate the condition needed for minimization of this error against temperature change.Accepted versio
In this paper we investigate the effects of stiffness, damping and temperature on the performance of...
The driving speeds at which self-excited motions occur in rotor-bearing systems are commonly referre...
The main property of gyroscopic devices is maintaining the axis of a spinning rotor, a mathematical ...
This paper considers the dependence of the rotor tuning condition of a rotor-vibratory gyrosc...
Influence of the elastic properties of the spring element on the rotor tuning condition of a rotor v...
The zero bias stability, which is an important performance parameter for vibratory cylinder gyroscop...
This thesis document was issued under the authority of another institution, not NPS. At the time it...
The uneven mass distribution of gyro rotors results in vibration, rotation and drift of gyro rotors,...
Gyroscope devices are primary units for navigation and control systems in aviation and space enginee...
The equations of motion of a heavy rotor attached to a massless horizontal shaft with unequal cross-...
This paper deals with the investigation of optimum values of the stiffness and damping which connect...
Abstract: The recent publications about gyroscope effects explained their physics and described them...
© Published under licence by IOP Publishing Ltd.A mathematical model of the rotor vibratory gyroscop...
Most of the current research activities in micromachined gyroscope are focusing on the design of a s...
Abstract. Simplify the gyro rotor into a hollow disk, each particle in the disk circular motion arou...
In this paper we investigate the effects of stiffness, damping and temperature on the performance of...
The driving speeds at which self-excited motions occur in rotor-bearing systems are commonly referre...
The main property of gyroscopic devices is maintaining the axis of a spinning rotor, a mathematical ...
This paper considers the dependence of the rotor tuning condition of a rotor-vibratory gyrosc...
Influence of the elastic properties of the spring element on the rotor tuning condition of a rotor v...
The zero bias stability, which is an important performance parameter for vibratory cylinder gyroscop...
This thesis document was issued under the authority of another institution, not NPS. At the time it...
The uneven mass distribution of gyro rotors results in vibration, rotation and drift of gyro rotors,...
Gyroscope devices are primary units for navigation and control systems in aviation and space enginee...
The equations of motion of a heavy rotor attached to a massless horizontal shaft with unequal cross-...
This paper deals with the investigation of optimum values of the stiffness and damping which connect...
Abstract: The recent publications about gyroscope effects explained their physics and described them...
© Published under licence by IOP Publishing Ltd.A mathematical model of the rotor vibratory gyroscop...
Most of the current research activities in micromachined gyroscope are focusing on the design of a s...
Abstract. Simplify the gyro rotor into a hollow disk, each particle in the disk circular motion arou...
In this paper we investigate the effects of stiffness, damping and temperature on the performance of...
The driving speeds at which self-excited motions occur in rotor-bearing systems are commonly referre...
The main property of gyroscopic devices is maintaining the axis of a spinning rotor, a mathematical ...