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Micromachined Angular Rate Sensor Applications Stabilization
Top Searches for this datasheetGYROCHIPModel QRS11 Micromachined Angular Rate Sensor Applications Stabilization Satellite Communication Antennas Optical Line-of-Sight Systems Missile Seekers Description GyroChipModel QRS11 "MEMS technology, solid-state "gyro chip." This input/high-level output device fully self contained, extremely small lightweight. external support electronics required. Since inertial sensing element comprised just micromachined piece crystalline quartz moving parts), virtually "unlimited" life. Model QRS11 mature product high volume production. fully qualified used numerous advanced aircraft, missile, space systems. Controls Aircraft Missile Flight Control Attitude Control Dampers Features High-Performance Inertial Sensor Compact, Rugged Package Long Operating Life Over 100,000 Hours MTBF Internal Electronics Input/High Level Output Wide Bandwidth Fast Start-Up Guidance Missile Mid-Course Guidance Inertial/GPS Navigation Systems Operation GyroChipModel QRS11 utilizes piece, micromachined, vibrating quartz tuning fork sensing element. Applying Coriolis effect, rotational motion about sensor's input axis produces voltage output proportional rate rotation. piezoelectric quartz material simplifies active element resulting exceptional stability over temperature product life. Instrumentation Rocket Boosters Simulation Training Aids GyroChip SYSTRON DONNER INERTIAL DIVISION applications assistance more information Systron Donner Inertial Division's micromachined inertial sensors, Call 1-800-227-1625. GYROCHIPModel QRS11 Micromachined Angular Rate Sensor .005[.127] .755 [19.18] PARAMETER Part Number Performance Level Power Requirements Input Voltage Input Current Input Power Noise Limits Performance SUMMARY SPECIFICATIONS QRS11-0XXXX-100** QRS11-0XXXX-101** Standard High [41.53] MOUNTING FLANGE [38.10] NAMEPLATE regulation 80mA (each supply) mVrms wideband, except ±0.5 KHz, mVrms PINS PLACES 0.640 [16.38] .032 [0.81] Standard Ranges Full Range Output (Nominal) Scale Factor Calibration 22°C) Scale Factor over Temperature (Dev. from 22°C) Bias Calibration 22°C) Bias Variation over Temperature (Dev. from 22°C) Short Term Bias Stability (100 const. temp) Long Term Bias Stability year) Sensitivity Start-Up Time Bandwidth (-90°) Non-Linearity Threshold/Resolution Output Noise 100Hz) Operating Life Environments Operating Temperature Storage Temperature Vibration Operating Vibration Survival Shock Weight AVAILABLE OPTIONS Special Ranges Extended Bandwidth Values indicated ±100°/sec range. ±50, 100, 200, 500, 1000°/sec ±2.5 value 0.03%/°C 2.0°/sec* 1.80°/sec* 0.5°/sec* 0.35°/sec* 0.002°/sec* 0.2°/sec 0.02°/sec/g 0.05% F.R. 0.004°/sec* 0.010°/sec/Hz* years, typical .040 [1.02] .050 [1.27] .530 [13.46] .005[.127] NOTES: QRS11 SUPPLIED WITH MOUNTING RINGS, MOUNTING SCREWS MATING TEST CONNECTOR. ANGULAR RATE APPLIED SHOWN WILL PRODUCE POSITIVE OUTPUT (NOT MARKED UNIT). UNIT MEASURE INCHES/[MM]. VOLTAGE INPUT (±4.0 MAX.) APPLIED SELF-TEST WILL RESULT CORRESPONDING PROPORTIONAL OUTPUT VOLTAGE. COMPATIBLE OUTPUT SIGNAL (REFERENCED POWER GROUND) INDICATING PROPERLY FUNCTIONING UNIT. QRS11-XXXXX-XXX Solder Assignment Connection, Leave Open Self Test Input +Vdc Input Power Ground Output -40°C +80°C -55°C +100°C grms random (Consult factory other vibration level requirements) grms random, minutes/axis axis grams Noise Flying Leads Extended Temperature Range "XXXX" designates range. SYSTRON DONNER INERTIAL DIVISION DIVISION HEADQUARTERS Systron Donner Inertial Division 2700 Systron Drive, Concord, 94518-1399 Tel: 1-925-671-6400 1-800-227-1625 Fax: 1-925-671-6590 E-mail: service@systron.com World Wide Web: http://www.systron.com EUROPEAN HEADQUARTERS Systron Donner Inertial Division Evegate Business Centre, Evegate Park Barn Smeeth Ashford, Kent, England TN25 Tel: ++44 1303 812778 Fax: ++44 1303 812708 E-mail: systron@easynet.co.uk Connection, Leave Open Rate Output Signal Ground -Vdc Input Case Ground subsidiary TECHNOLOGIES, INC. ©1998 Systron Donner Inertial Division. GyroChip registered trademark Sensors Systems Company. rights reserved. Printed U.S.A. DS01-2 9/98 Other recent searchesT2000 - T2000 T2000 Datasheet SB106 - SB106 SB106 Datasheet 138P125-W-Ag - 138P125-W-Ag 138P125-W-Ag Datasheet RT3P66M - RT3P66M RT3P66M Datasheet HS-1450 - HS-1450 HS-1450 Datasheet CX24430 - CX24430 CX24430 Datasheet CA3086 - CA3086 CA3086 Datasheet BVU-559TT9 - BVU-559TT9 BVU-559TT9 Datasheet 74LVX16374 - 74LVX16374 74LVX16374 Datasheet
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