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Thermal Imaging Device (9000J)
GPS-Aided Inertial Navigation Systems
Compact MEMS/FOG inertial units with multi-GNSS support, RTK-level accuracy, and reliable navigation in GNSS-denied conditions.
Key Features:
✔️ Form factors from 82 × 40 × 26 mm / 200 g to 120.5 × 53.2 × 49.3 mm / 220–320 g
✔️ Multi-GNSS: GPS, GLO, GAL, BDS, QZSS with RTK/PPK/PPP/DGPS/SBAS
✔️ 1 cm RTK position accuracy; 2.5 cm PPP and 60 cm SBAS options
✔️ Heading accuracy 0.08° (dual-antenna) to 1° (single-antenna static)
✔️ Pitch/roll accuracy 0.03–0.05° for precise attitude control
✔️ MEMS or FOG IMUs with gyro/accelerometer/compass sensor fusion
✔️ Maintains navigation with 0.2% distance-travelled error in GNSS denial
✔️ Embedded or external magnetic compass for heading independent of satellites
✔️ Supports UAVs, UGVs, rotorcraft, agriculture systems, and survey mapping
✔️ Models include INS-U, INS-B, INS-P, INS-D/DL/DM/FI for varied performance tiers
Category: Detectors
Tags: Gps aided inertial navigation systems price, GPS-Aided Inertial Navigation Systems, GPS-Aided Inertial Navigation Systems (INS), Inertial navigation system, Inertial Navigation System price
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GPS-Aided Inertial Navigation Systems
The GPS-Aided Inertial Navigation Systems line integrates MEMS-based and FOG-based inertial measurement units with tactical or industrial-grade performance since 2001. Compact form factors range from 82 × 40 × 26 mm (INS-U at 200g) to 120.5 × 53.2 × 49.3 mm across models INS-B, INS-P, and INS-D variants weighing 220–320 grams. Multi-constellation GNSS receivers support BDS, GAL, GLO, GPS, and QZSS with correction methods including RTK, PPK, PPP, DGPS, and SBAS. Embedded or external magnetic compass options provide heading determination independent of GNSS availability during signal denial conditions.
Position accuracy reaches 1 cm RTK across all standard models with 2.5 cm PPP and 60 cm SBAS alternatives. Heading accuracy spans from 0.08° dual-antenna performance on high-grade models (INS-D, INS-DM, INS-FI) down to 1° single-antenna static capability. Pitch and roll measurements achieve 0.03–0.05° dynamic accuracy enabling precise attitude control. The systems integrate gyroscope, accelerometer, and compass data through sophisticated sensor fusion algorithms maintaining accuracy during extended GNSS-denied navigation with demonstrated 0.2% position error over distance travelled performance.
Military and civilian operators deploy the GPS-Aided Inertial Navigation Systems across fixed-wing UAV navigation, autonomous ground vehicle guidance, and rotorcraft stabilization. Emergency response teams utilize models INS-P and INS-B for disaster reconnaissance in GPS-challenged urban canyons and underground environments. Precision agriculture applications rely on INS-DL models for autonomous tractor guidance and field mapping accuracy. Surveying professionals employ dual-antenna variants for real-time heading determination during mapping operations.
Tactical Supply Pakistan supplies inertial navigation solutions meeting MIL-STD-810G and MIL-STD-461 compliance standards through this comprehensive GPS-aided system family. Organizations achieve robust multi-domain positioning and orientation capability across GNSS-enabled, contested, and GPS-denied operational environments.
Can GPS-Aided Inertial Navigation Systems maintain accuracy without satellite signals?
Yes, integrated inertial sensors sustain navigational accuracy during extended GNSS denial using onboard gyroscope and accelerometer dead reckoning with demonstrated position accuracy of 0.2% over distance travelled when calibrated and initialized with known coordinates.
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