HG1930 Inertial Measurement Unit
The HG1930 is a MEMS based IMU designed to meet the needs of a range of applications including ground and oceanographic surveying, robotics, commercial camera stabilization, control and navigation of unmanned aerial vehicles, missiles, munitions and projectiles. The HG1930 includes MEMS gyroscopes and accelerometers that are environmentally sealed in a rugged aluminum housing. In addition, it employs an internal environmental isolation system to attenuate unwanted inputs. Three different performance grades of the HG1930 are available off-the-shelf. The HG1930 offers many configurable features, such as data rate output and flight control filtering, to simplify system integration. We design, develop and manufacture all of the MEMS inertial sensors utilized in the HG1930 IMU. All of this culminates in the HG1930 providing industry leading MEMS sensor performance while maintaining minimal SWAP parameters. The HG1930 is designed and built at a Honeywell facility in the USA. It typically has an ECCN of 7A003.d.1 but can vary depending on model selected. It generally requires an export license
The HG1930 includes MEMS gyroscopes and accelerometers that are environmentally sealed in a rugged aluminum housing. In addition, it employs an internal environmental isolation system to attenuate unwanted inputs. Three different performance grades of the HG1930 are available off-the-shelf. The HG1930 offers many configurable features, such as data rate output and flight control filtering, to simplify system integration.
We design, develop and manufacture all of the MEMS inertial sensors utilized in the HG1930 IMU. All of this culminates in the HG1930 providing industry leading MEMS sensor performance while maintaining minimal SWAP parameters.
The HG1930 is designed and built at a Honeywell facility in the USA. It typically has an ECCN of 7A003.d.1 but can vary depending on model selected. It generally requires an export license
Specifications
| Performance: Accelerometer Sensor Technology | MEMS |
| Performance: Accelerometer Operating Range | up to 85g in X axis, 35g in Y and Z |
| Performance: Accel Bias Repeatability (mg 1σ) | .05 |
| Performance: Accel Bias In-Run Stability (mg 1σ) | 0.02 |
| Performance: Gyro sensor technology | MEMS |
| Performance: Gyro Operating Range | up to 7,200°/sec (X axis) , 1,440°/sec (Y and Z axes) |
| Performance: Gyro Bias Repeatability | 7 °∕hr 1σ |
| Performance: Gyro Bias In-Run Stability | .025 °∕hr 1σ |
| Performance: Gyro ARW | 0.125 (Roll) 0.095 (Pitch and Yaw) |
| Performance: Accel Velocity Random Walk (VRW) | 0.03 |
Tell us your accuracy, environment, and integration requirements and we'll recommend the right board and correction approach.