Gyroscopes
Measure or maintain a single distance in relation to an object, regardless of shift in angle.
See Also: IMU, Accelerometers, Flywheel
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Rugged Package
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Inclinometers, Accelerometers, Gyroscopes, IMU, and AHRS Ruggedized Systems
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Directional Gyroscope
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A flight instrument used in an aircraft to inform the pilot of the aircraft's heading.
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Bench-Top Type ASE Light Source
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ASE(Amplified Spontaneous Emission) light sources are low-coherent light sources ,which combines the both features of high intensity like laser and broad spectrum like LED. Output stability is greater than those of LD and LED, and therefore they are suitable for high accuracy measurement applications. With the use of rare-earth-doped fluoride fibers, the plentiful lineup of FiberLabs light sources includes the 540 nm-, 850 nm-, 1300 nm-, 1480 nm- and SCL-bands that other companies do not provide.They are the best light sources for FBG sensors, OCT, fiber optic gyroscopes, gas sensors, and fluorescence excitation, as well as for measurement of optical components. The bench-top type is easy to use as a stand-alone light source and the modular type is convenient for integration into equipments.
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Standard Directional Gyroscopes
4000B-series
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The 4000B is our standard air-driven directional gyro. As the aircraft turns left or right, gears on the sensing unit and dial shaft translate this rotation into rotation of the instrument’s vertical dial. Left turns produce clockwise dial rotation and right turns produce counter-clockwise rotation. The gyro is controlled by a heading selector knob located on the lower left of the instrument. Pressing and turning the knob first disengages the dial shaft and then resets the dial to a new heading, which results in a new course indication. Releasing the selector knob re-engages the dial shaft. The on-course position of the pointer is always at the top of the azimuth circle (0° on the dial with the aircraft headed north).
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Weapons Orientation Modules
WOM
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The WOM™ weapon orientation modules provides a level of performance previously unseen in the world of miniature 3DOF orientation systems. WOM™ employs the use of three axes each of gyroscopes, accelerometers, and magnetometers to track both slow and fast movements of weapons in real-time. It houses propriety calibration techniques for soft- and hard-iron interference that are specific to the different weapon classes on which it can be used. Calibrations are able to be performed quickly and easily by minimally trained individuals without requiring any precise movements.
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Inertial Navigation Systems
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An inertial navigation system (INSAn INS or Inertial Navigation System - sometimes used synonomously with IMU is a device used to measure a vehicle's speed, position, velocity, heading and orientation by using an accelerometer and a gyroscope.) is a high-tech navigator using motion and rotation sensors alongside a computer to figure out where something is, how it’s moving, and how fast. By using dead reckoning, the INS method for knowing positioning, it continuously calculates an object’s position and orientation based on its initial location. This allows users in airplanes, submarines, or even spacecrafts to guide and keep track of their location without signals such as GPSGlobal Positioning System is a navigation satellite system. See also.
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4000B ARINC-style Directional Gyroscopes
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This instrument was developed for those pilots that prefer the distinct, professional look of an ARINC-styled cockpit. It is identical to the standard 4000B model differing mainly in aesthetics. Besides its distinct bezel and airplane, the display graphics and colors differentiate it from the standard model. A heading reminder bug is available as an option.
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Heading Reference Directional Gyroscopes
4000HR-series
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The 4000HR air-driven directional gyro offers some of the best features of our other popular models. It inherited all of the functionality and reliability of the industry standard 4000B upon which it’s based, and it picked up a heading reference bug from the 4000C autopilot model.
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Gyroscope Module 3-Axis L3G4200D
27911
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The Gyroscope Module 3-Axis L3G4200D provides raw angular rate and temperature data measurements that are accessed from the selectable digital I2C or SPI interface. The small package design and SIP interface accompanied by the mounting hole make the sensor easy to integrate into your projects. Designed to be used with a variety of microcontrollers, the module has a large operating voltage window.
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Standard Attitude Gyroscopes
5000B-series
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The 5000B is an air-driven gyro that has a pictorial horizon mask and fixed airplane. The mask moves to indicate climb, dive, and bank. Bank and pitch attitudes are displayed so that the pilot’s sensing of the gyro indication is the same as the interpretation of the relation between the wings of the aircraft and the natural horizon during visual flight.
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Rate & Inertia Sensors
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TE Connectivity (TE) provides electronic test and measurement systems, such as inertial sensors, rate sensors, and rate gyroscopes for demanding industrial, military, aerospace, automotive crash testing, robotics, biomechanics, and more.
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Autopilot Attitude Gyroscopes
5000E/L-series
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The 5000E air-driven attitude gyro is another variation of our standard 5000B model. It includes inductive pickoffs that generate the signals necessaryto drive an autopilot. The intuitive display has a moving horizon mask that indicates the position of the aircraft’s wings in relation to the natural horizon. This attitude information is passed along to the autopilot system.
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Gyro Pressure
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Used to monitor the vacuum developed in the system that actuates the air driven gyroscopic flight instruments.
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Programmable Sensor Module With CAN Connection
PCAN GPS
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The PCAN-GPS is a freely programmable sensor module for position and attitude determination. It has a satellite receiver, a magnetic field sensor, an accelerometer and a gyroscope. The recorded data can be transmitted on a CAN bus and logged on the internal memory card. The data is processed by a microcontroller from the NXP LPC4000 series.
