Showing results: 31 - 45 of 51 items found.
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MS-IMU3020 -
MEMSense, LLC
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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Revolution GS -
True North Technologies
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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4000C/D-series -
Sigma Tek, Inc.
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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4000HR-series -
Sigma Tek, Inc.
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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Rebel CT4 -
Influx Technology LTD
The Influx Rebel CT 4 is a compact data logger, making it an ideal choice for engineering applications that require vehicle CAN 2.0 and LIN network data. The Rebel CT 4 can optionally be expanded to include GNSS , 3D accelerometer, 3D Gyro, Wi-Fi and 4G LTE.
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MK31 INS -
Teledyne Marine TSS
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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LinkQuest Inc.
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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STI3000 -
Solidus Technologies, Inc.
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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5000E/L-series -
Sigma Tek, Inc.
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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4000H-series -
Sigma Tek, Inc.
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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SATURN INS -
Teledyne Marine TSS
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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CoventorWare -
Coventor
CoventorWare is an integrated suite of design and simulation software that has the accuracy, capacity, and speed to address real-world MEMS designs. The suite has many MEMS-specific features for modeling and simulating a wide range of MEMS devices, including inertial sensors (accelerometers and gyros), microphones, resonators, and actuators. The included field solvers provide comprehensive coverage of MEMS-specific multi-physics, such as electrostatics, coupled electro-mechanics, piezoelectric, piezoresistive, and damping effects.
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Metis -
Afore
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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Safran Federal Systems
Safran Federal Systems is now one of the only companies with a full complement of PNT technologies with the addition of proven inertial navigation solutions.Hemispherical Resonator Gyro (HRG) Crystal™ technology leverages state of the art manufacturing and offers revolutionary performance and reliability over existing technologies, for tactical to strategic applications across all domains. With more than 30,000 HRGs produced and over 15 million operational hours, the technology is proven and tested in military applications worldwide.
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Data Patterns Pvt. Ltd.
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.