Miniature MEMS Quartz GPS/INS Ideal for High-Precision Civil & Military Applications: • • • • • • • • Targets & Drones Position & Orientation System Stabilization UAVs & Other Unmanned Vehicles Range Instrumentation Commercial Aviation Navigation Railroads Helicopter Extremely Small Size Integrated INS/GPS Optimized 28-State Kalman Filtered Navigation Solution RS-232 Digital Interface Low Power Consumption (<5W) Accepts External Magnetometer Data for Heading Reference In-Air Dynamic Alignment Capability1 The MMQ™G offers a unique combination of the Systron Donner Inertial solid-state Inertial Measurement Unit (IMU) and the Jupiter PICO™ commercial Global Positioning System (GPS) receiver. The MMQ™G's MEMS quartz rate sensors and MEMS accelerometers make up an IMU system that is tightly coupled with the Jupiter's 12-channel Coarse/Acquisition (C/A) Code GPS engine to provide a highly accurate navigation solution. The MMQ™G also accepts 3-axis magnetometer data, which it uses as a heading reference in order to improve heading stability. This also allows for alignment during low dynamic motion, as experienced in ocean applications. A “heading hold” feature allows delayed takeoffs after alignment is complete. The MMQ™G combines tremendous performance and versatility with an extremely compact size and low weight at a very low price. Leveraging the C-MIGITS® III user-friendly message based navigation outputs, the MMQ™G provides a powerful solution for Guidance, Navigation & Control. 1 In-Air dynamic alignment without magnetometer reference requires system velocity below 95 kts.

Miniature MEMS Quartz GPS/INS 1.88” (47.6 mm) Size (Vol.) Weight Power I/O 9.0 in <0.50 lbs (<0.227 kg) + & - 12Vdc at <5W total RS-232, output protocol similar to GPS-153 Navigation Performance (C/A Configuration) Position (SEP) Random Walk Velocity (1σ) Attitude (1σ) (In Dynamic Motion) Heading (1σ) (In Dynamic Motion) Time (1σ) Range Bias Turn-on to Turn-on Stability (fixed temp) Bias In-Run Stability (at any temperature) Bias Instability Angle Random Walk Scale Factor Error Alignment Bandwidth (-90°Phase Shift) Range Bias Turn-on to Turn-on Stability (fixed temp) Bias In-Run Stability (at...