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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Product
INERTIAL MEASUREMENT UNIT
MS-IMU3020
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The MS-IMU3020 delivers market leading price to performance in an ultra-compact aluminum package. The gyro bias instability of 0.9 /h and accelerometer bias instability of 9 g supply ample performance to support a range of applications from UAS navigation and control to pipeline inspection.
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Product
Gyro Test Panel
TA-256
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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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Product
Accelerometer & Platform Test Bench
mS 1115
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Platform Test Bench used to test the Digital Inputs, Accelerometer Count Reading, High and Low Gyro Torque control of Platform. It also performs Real Time Test for single negative pulse, checks Roll Axis, Pitch Axis, Azimuth Axis. Software package is available to test the Accelerometer.
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Product
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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Product
Autopilot Directional Gyroscopes
4000C/D-series
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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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Product
Acceleration and Gyro Sensors
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Acceleration and gyro sensors specifically for the motorsports industry.
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Product
Wafer Probe Test System
STI3000
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The STI3000 is a wafer-level MEMS and mixed signal ASIC probe test system that combines several functional STI test equipment blocks for testing gyros, accelerometers, pressure sensors, microphones, resonators, and mixed signal ASICs.
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Product
Next Generation Subsea Inertial Navigation Systems
TOGSINS
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The new TOGSINS builds on core TSS fibre optic gyro technology by incorporating inertial navigation (INS) capability. As with TOGS, it is available in three standard heading accuracy variants: 0.1° (TOGSINS1), 0.3° (TOGSINS3) and 0.5° (TOGSINS5), all rated for operational depths to 4,000m or 6,000m giving you a range for all your needs.Inertial position data is produced using an INS algorithm, within the firmware framework of TOGS, whilst attitude data is delivered via accurate roll/pitch measurement of 0.01° (TOGSINS1) and 0.05° (TOGSINS3 and TOGSINS5), and a heave performance of 5cm or 5%.
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Product
Electronic Compass for Dynamic Conditions - Vibration, Acceleration, Uneven Terrain, or Rough Seas
Revolution GS
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If your compass application involves vibration, acceleration, uneven terrain, or rough seas, you will find the True North Revolution GS electronic compass to be an uncompromising solution that will outperform rival units costing considerably more. The GS provides remarkably accurate heading, pitch, and roll in dynamic conditions. It all starts with a precision 3-axis solid-state magnetometer. Two angular rate gyros independently stabilize pitch and roll. They augment a dual-axis electrolytic tilt sensor that provides precise tilt measurements in static environments. Two sets of independent filters, one set for pitch and one for roll, combine gyro and electrolytic sensor measurements to provide the best available tilt measurements.
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Product
KMD540 Series and RDR2000/2100 Panel
TA-3C
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The TA-3C test fixture is a combination of the KMD540 testing requirements and the RDR-2000/2100 weather radar interface requirements. This panel allows the technician to test the KMD540 MFD as a stand alone item (with external simulators) or together with a radar sensor for a dynamic real time test. The panel includes the required switching for sensor alignment and KMD testing along with input jacks for the required data inputs. Also built into the fixture is an analog gyro simulator for checking the stabilization functions of the sensor. The full enclosure comes in standard panel width.
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Product
Accelerometor, Gyro, Magnetometer Breakout Board
SEN-38001
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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.
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Product
Collins Radar Fixture with Gyro Simulator
TA-3A/B
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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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Product
XYZ Bootstrap Directional Gyroscopes
4000H-series
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Sigma Tek's Directional Gyro with heading synchro output provides a cost effective link to "bootstrap" other instruments requiring heading information for: display orientation to aircraft heading, heading stabilization functions, and other navigational calculations and/or solutions. Specific applications include: Argus Moving Map Display®, L-3 Avionics Stormscope®, and Insight Strike Finder®.
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Product
Gyro Evaluation & Test Equipment
MS 1113
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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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Product
Electric Attitude Gyroscopes
5000EG-series
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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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Product
ESI(Electronics Systems Integration Unit)
MS 2004
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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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Product
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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Product
Noise Board
332D-11 VG
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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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Product
Gyro Sensors For General-Purpose
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Panasonic Industrial Devices Sales Company of America
Gyro Sensors For General-Purpose
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Product
Gyro Sensors (Automotive Only)
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Panasonic Industrial Devices Sales Company of America
Panasonic offers Gyro Sensors (Automotive Only) for navigation, navigation inclined detection and rollover detection.
