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Gyros
measure or maintain a single distance in relation to an object, regardless of shift in angle.
See Also: Accelerometers, Navigation
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Next Generation Subsea Attitude and Heading Reference Systems
TOGS
The new TOGS subsea navigation system is built on core TSS fibre optic gyro (FOG) navigation technology with significant improvements in efficiency and functionality. It is available in three standard heading accuracy variants: 0.1° (TOGS1), 0.3° (TOGS3) and 0.5° (TOGS5), all rated for operational depths to 4,000m or 6,000m. Attitude data is delivered via accurate roll/pitch measurement capabilities of 0.01° (TOGS1) and 0.05° (TOGS3 and TOGS5), and a heave performance of 5cm or 5%.
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Noise Board
332D-11 VG
This printed circuit board was designed to original specifications and contains OEM specified parts. This board is required for testing the 332D-11 series gyros. Also contained on board is the Method A type calibration and sample and hold circuits required to perform the calibration of the noise circuits.
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Precision Marine Geodetic Systems
Using leading-edge "Broadband Acoustic Spread Spectrum Technology", accurate sound wave traveling time between LinkQuest's subsea precision transponders and surface station can be measured. When the system is integrated with a Kinematic GPS, motion sensors and a gyro on the surface vessel or undersea vehicle, sub-centimeter acoustic positioning can be achieved.
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Gyro Evaluation & Test Equipment
MS 1113
The automatic test bench for gyros (ATP) is used to carry out the final acceptance test for the gyros in the stand-alone mode. It is a PC based test set up incorporating standard and custom built test and measuring instruments interfaced by GPIB bus. The gyros are installed on the platform, which is used to provide information pertaining to the angle at which aircraft is flying.
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Autopilot Attitude Gyroscopes
5000E/L-series
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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Acceleration and Gyro Sensors
Acceleration and gyro sensors specifically for the motorsports industry.
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MEMS Gyro Sensors For Consumers
Panasonic Industrial Devices Sales Company of America
MEMS Gyro Sensors For Consumers
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Gyro Sensors For General-Purpose
Panasonic Industrial Devices Sales Company of America
Gyro Sensors For General-Purpose
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Gyro Sensors (Automotive Only)
Panasonic Industrial Devices Sales Company of America
Panasonic offers Gyro Sensors (Automotive Only) for navigation, navigation inclined detection and rollover detection.
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Instrument Test Unit
Instrument Test Unit For Advanced Inertial Sensors (INTU) is used for testing and evaluation of Ring Laser Gyro (used in GSLV/PSLV launch vehicles), that detects the angular displacement during rotation. The INTU receives displacement signals from the sensor (RLG) to evaluate the sensor characteristics and also generates signals required towards initiating the action of the sensor.
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Gyro Sensors For General-Purpose(2)
Panasonic Industrial Devices Sales Company of America
Gyro Sensors For General-Purpose(2)
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Laboratory Centrifuges
Centrifuge systems are designed for the development, test, evaluation and calibration of accelerometers and a variety of inertial devices. Centrifuges provide a cost-effective solution for simulating high-"G" environments in the laboratory. They support testing of devices such as MEMS-based Inertial Measurement Units (IMUs), low-cost quartz or silicon sensors, Ring Laser Gyros (RLGs), Fiber-Optic Gyros (FOGs), fuzes and crash sensors.
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Ring Laser Inertial Navigation and Weapon Stabilization System for Defense Applications
MK31 INS
The MK31 is a ring laser gyro (RLG) inertial navigation system that provides accurate heading, attitude and positional data for a wide range of naval vessels including frigates, patrol vessels and submarines. It is ideal for customers seeking a cost-effective and reliable solution for navigation and control of onboard radar, weapon, and satellite systems.
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Standard Directional Gyroscopes
4000B-series
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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5000B-series Attitude Gyroscopes With Warning Flag
This gyro is a variation of our popular 5000B air-driven attitude gyro. It includes a warning flag that drops into view upon the loss of vacuum. This can be a life saving feature during an emergency in a busy cockpit. The horizon mask moves to indicate climb, dive, and bank attitudes, which are portrayed against a fixed airplane. The fluid movements and intuitive presentation provide the pilot with a realistic sense of the aircraft’s attitude in relation to the natural horizon.
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Standard Weather Radar Test Panel
TA-3
Universal weather radar test panel with integral gyro simulator and monitor jacks. Discrete test jacks for common signals, altitude select switches and a dedicated connector for the RDS series radars. Click on picture for larger view.
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MEMS Gyro Sensors For Rollover Detection
Panasonic Industrial Devices Sales Company of America
MEMS Gyro Sensors For Rollover Detection
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PMA’d Mechanical Gyro Suction Gauge
Is designed to save space in cockpit panels. It utilizes an internal diaphragm to read directly from the source for accuracy and reliability.
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Motion Simulator For Test Systems
Metis
METIS is a motion simulator for sensor and end system level testing. Configurable design allows you to create system you need! - 1-axis rate table for gyro testing - 2-axis unit for 6DOF accelerometer and gyroscope testing - 3-axis Gimbal system for simultaneus Yaw, Pitch and Roll stimulus.
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DGS-65 Test Panel with FV Simulator / Bed of Nails
TA-650
The TA-650 is a new test fixture that will give any instrument shop the ability to conduct more detailed testing of the Collins DGS-65 directional gyro then was previously available.
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Flight Instruments & Gyro Department
Aero Instruments & Avionics, Inc.
The Flight Instruments & Gyro Department offers complete functional testing, repair and overhaul of most instruments & gauges located within the aircraft cockpit, and the associated computers that control them.
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Cageable Attitude Gyroscopes
5000M-series
The 5000M 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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Electric Attitude Gyroscopes
5000EG-series
The 5000EG gyro is based on our air-driven 5000B model, whose proven reliability has made it the industry standard for many years. There are two models available: 14 and 28 VDC. The rotor is precisely machined from a heavy-metal tungsten alloy, which has a higher mass than brass, contributing to the instrument’s demonstrated stability. The electric motor is driven by a built-in power inverter, and has an integrated air-erection mechanism. A warning flag is deployed upon loss of primary power. During acrobatic flights or short stops, the gyro’s mechanism can be caged whenever the knob is pulled.
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Heading Reference Directional Gyroscopes
4000HR-series
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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ESI(Electronics Systems Integration Unit)
MS 2004
The ESI subsystem provides platform interfaces like Gyro and on board Radar Blanking. This unit receives Analog and Digital GYRO inputs from ship and pre- trigger pulses from on board radars of the ship. This unit measures and provides the ship heading data to VARUNA ESM system. It also provides Heading, Roll and Pitch data to the ECM system. This unit also generates band wise composite ESM Rx. Blanking gates and provides all the required interfaces to ESM receiver, ECM System and System Controller units.
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Collins Radar Fixture with Gyro Simulator
TA-3A/B
This weather radar test fixture is a combination of the established WXT-250 series fixture and the RDR-2000 and RDR-2100 radars so that a single panel will provide many features that are still required today. The gyro simulator built into the panel is usable for either radar being tested and eliminate's plugging in any external simulator. The features for both product lines as shown in their respecting CMM's are provided on the panel so that full testing and alignment of these radars and their system components can be tested and/or evaluated. If you require any changes or other product versions please give us a call.
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Autopilot Directional Gyroscopes
4000C/D-series
The 4000C/D is an air-driven directional gyro with A.C. autopilot pickoffs. Left turns produce clockwise dial rotation and right turns produce counter-clockwise rotation. Two knobs control the gyro. The left knob is used to cage the unit, and the right knob is used to select the instrument’s heading. To change course, the right selector knob is pressed and turned to disengage the dial shaft and set the pointer to a new heading. Releasing the selector knob re-engages the pointer with the dial shaft. As the aircraft turns onto a new course, the pointer returns to its original position. 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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High Accuracy Fibre Optic Inertial Navigation System
SATURN INS
SATURN INS, from Teledyne TSS, is a world leading surface navigation system which offers enhanced unparalleled INS performance which builds on the TSS fibre optic gyro system by adding inertial navigation (INS) capability.As with SATURN, it is available in three standard heading accuracy variants; 0.1° sec lat (SATURN10INS), 0.3° sec lat (SATURN30INS) and 0.5° sec lat (SATURN50INS).
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Gyro Test Panel
TA-256
Designed to test the KI256 / KI258 panel mounted Flight Director gyros. The panel contains a power supply, the special manufacturers recommended rate board required by SA-103 to properly verify outputs As well as all other electronics required to support by the book testing.
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Accelerometor, Gyro, Magnetometer Breakout Board
SEN-38001
The LSM9DS1 is a highly configurable, flexible and precise motion sensing solution from ST Microelectronics - the latest in a wide-ranging inertial product line. It integrates a 3-axis accelerometer, 3-axis gyroscope and 3-axis magnetometer into a single IC , giving you a full nine degrees of freedom (9-DOF) in a tiny 3mm x 3.5mm package. Even with support components, square mounting pattern and connection breakouts for both SPI and I2C, this board is barely the size of a quarter.
