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7011 / 7012 Inertial Reference
 
Feature Highlights
  • Precision Strap Down Inertial Reference for Lateral and Normal Sensing
  • Direct replacement for LVDT based accelerometers
  • MEMS Technology
  • High Sensitivity
  • Low Temperature Drift
  • Low Cross-Axis Sensitivity
  • Full Operation Over -50º to 70º C
  • Includes EMI Filter, Power Supply, MEMS Sensor, Amplifier, Filter and Output Buffer
  • Self Test
  • 26 VAC Power (MIL-STD-704A)
  • MTBF 70,000 hours (MIL-HDBK-217)
  • Tested to MIL-STD-810 and MIL-STD-461/462

Inertial Reference

Description

The 7011 / 7012 inertial reference provides a strap down lateral or normal accelerometer for spatial orientation measurements as part of a complete inertial reference autopilot system. The units are designed to replace aging mechanical LVDT based accelerometers with superior performance. The units deliver optimal performance in MIL-SPEC environments. The 7011 / 7012 Include:

Output: The 7011 / 7012 has a ratiometric AC voltage output. Output is proportional to both the 28 VAC power and the acceleration sensed. This response exactly duplicates the response from LVDT based accelerometers it replaces.
Power Supply: The 7011 / 7012 operates directly from 28 VAC Aircraft Power (MIL-STD-704). The unit handles the sags and surges common on the power bus including induced effects of lightning.
MEMS Sensing: The MEMS core of the 7011 / 7012 provides a solid state foundation for acceleration measurement. The MEMS accelerometer responds to ±1 g changes in the gravitational acceleration due to changes in aircraft orientation.
Amplification: For maximum resolution of acceleration data, the 7011 / 7012 amplifies signals with a multi-stage differential amplifier.
Filtering: The 7011 / 7012 filters and conditions signals with active low-pass filtering to eliminate unwanted signal components. Filter is a 17 Hz, 6-pole Bessel style.
Self-Test: The 7011 / 7012 contains a built-in self-test function. A signal line is available to engage the self-test remotely.
 

Applications

  • Inertial Reference
  • Autopilot Input
  • Tilt Monitoring


Electrical Performance: Vs = 26 VAC; Tc = 25º C unless otherwise specified

Parameter Min. Typ. Max. Units
Full Scale Measurement Range -1   +1 g
Sensitivity 0.2     mg
Cross Axis Sensitivity     0.3 % FSO
Null -4   +4 mg
Filter Cutoff Frequency (Six Pole Bessel)   17   Hz
Linearity   0.1   % FSO
Zero Offset Temperature Drift     0.007 % FSO / º C
Span Temperature Drift     0.054 % FSO / º C
Supply Voltage (Vs) (MIL-STD-704 compliant)   13.1 26   40.7 Volts AC
Operating Current   65   mA

 

Environmental Requirements: Vs = 26 VAC unless otherwise specified

Parameter Min. Typ. Max. Units
Operating Temperature -50   70 º C
Storage Temperature -55   85 º C
Humidity     100 %
Altitude     40,000 feet

 

Physical Specification:

Parameter Specification
Enclosure Type Environmentally and EMI Sealed Aluminum Enclosure
Enclosure Size 1.25" x 2.50" footprint (not including connector) 2.59" height
Weight 9 oz.
Connector

MS27508E10F99P

 

Datasheet in PDF

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