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Bilag 1: Helikopterens fysiske egenskaber - SmartData

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<strong>Bilag</strong> 3: Kommercielle IMU/AHRS<br />

Produkt-navn<br />

Producent<br />

LN-200<br />

NorthrupGrumman<br />

Crista IMU<br />

Cloud Cap<br />

Technology, Inc.<br />

TCM2-50<br />

Precision<br />

Navigation, Inc.<br />

MP2028g<br />

MicroPilot<br />

REV2.4.6DOFK<br />

Rotomotion, LCC<br />

REV2.5AHRSA<br />

Rotomotion, LCC<br />

3DM-DH<br />

Microstrain<br />

Beskrivelse Dimensioner<br />

Vægt<br />

6-DOF IMU<br />

fiber-optic gyroer<br />

Pris<br />

8.9cm x 8.9cm x 8.5 cm<br />

700.0 g<br />

Pris ukendt (“low-cost”)<br />

6-DOF GPS-aided IMU 1.35” x 1.50” x 0.80”<br />

18.9 g<br />

3-axis sensing instrument<br />

(accelerometre og<br />

magnetometre) +/- 50 o<br />

UAV autopilot (AHRS)<br />

IMU, GPS modtager<br />

100-field telemetry (1Hz)<br />

6-DOF IMU<br />

AHRS<br />

(gyroer, accelerometre og<br />

magnetometre)<br />

Microminiature Solid State 3axis<br />

Pitch, Roll, & Yaw Sensor<br />

1,950.00$<br />

63.5 x 50.8 x 31.75 mm<br />

45.5 g<br />

769.00$<br />

10 cm x 4 cm x 1.5 cm<br />

28.0 g<br />

5,000.00$<br />

Dimensioner og vægt ukendt<br />

300.00$<br />

Dimensioner og vægt ukendt<br />

2090.95$<br />

2.8cm x 6.7cm x 0.8cm<br />

Vægt ukendt<br />

795.00$<br />

Kilde<br />

http://www.ngnavsys.com/<br />

http://www.cloudcaptech.com/crista_imu.htm<br />

http://www.precisionnav.com<br />

http://www.micropilot.com/<br />

http://www.rotomotion.com<br />

http://autopilot.sourceforge.net<br />

http://www.rotomotion.com<br />

http://autopilot.sourceforge.net<br />

http://www.microstrain.com/3DM-DH.html

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