Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Group SASfiledCriticalAirbus Group SAS
Publication of GB1330550ApublicationCriticalpatent/GB1330550A/en
Study of a rotary-drive vibratory-output two-degree-of-freedom gyro(Design and performance of vibratory output gyro using asymmetrical rotor for rocket inertial attitude control)
MICRON- A strapdown inertial navigator using miniature electrostatic gyros(Low cost strapdown inertial navigator with miniature electrostically suspended gyros, discussing system performance goal in terms of position, velocity and attitude errors)
Stability of the stationary motions of a satellite with a gyroscope in a central Newtonian field(Stability of steady state motions of gyroscope mounted in Cardan suspension on satellite in circular orbit in Newtonian force field)
The motion of the axis of a gyroscope casing during the run-out phase for the case of nonperpendicularity of the axes of rotation of the rotor and of the inner ring of the Cardan suspension(Precession of gyroscope casing during run-out phase for case of nonperpendicularity of rotor rotation axis to inner gimbal ring)
Influence of friction in the suspension bearings on the motion of a gyroscope with forced rotation of the base(Influence of dry friction in suspension bearings on motion of gyroscope with forced gimbal rotation)