The NAVSYS modular GPS/Inertial software product is called InterNav. The InterNav software includes the functions shown in the block diagram, below, and is programmed in modular, ANSI-compliant C++ code to provide maximum flexibility for integration of different GPS and inertial components.

The InterNav Kalman Filter is designed to utilize various grades of IMU quality instruments via selectable parameters through a “configuration” file. This file provides the user with the flexibility to configure the overall system to customize the configuration for the GPS receiver and inertial sensor unit to meet customer-specific operational requirements, with minimal software modifications. These modifications only affect the interface structure with the GPS and IMU, while allowing the navigation and Kalman parameters to be either pre-programmed for a specific mission, or to be run-time configurable to optimize local application via the memory mapped configuration data. Additionally, many operational parameters can also be specified either through the operator interface or through the configuration file. These options include, but are not limited to: Kalman Filter update rates, initial location information, display window configuration, and data logging. To enable rapid reconfiguration of the Kalman Filter for integration with different inertial devices, key words are defined that are loaded at start-up to optimize the filter performance.

The InterNav software includes several software modules. The receiver interface module handles the interface to the GPS receiver. This receives and formats the GPS pseudo-range and carrier phase observations for processing in the Kalman Filter. The IMU interface module performs a similar function, formatting the IMU Dq (angle rate) and DV (acceleration) observation for the inertial navigation solution. The inertial navigation solution is based on a quaternion integration algorithm to compute the body-to-navigation transformation direction cosine matrix and integrate the acceleration to propagate position and velocity in a wander-azimuth navigation frame. The integrated GPS/inertial solution can also be precisely time aligned with other sensors including digital video products or laser rangefinders.

The InterNav software implements two different alignment modes, rough leveling and rough alignment, with different state definition. In the rough leveling mode (system state=1), the GPS updates are used to estimate where the local level frame is. Once local level has been determined, the system transitions to the rough alignment mode (system state=2) to generate an initial estimate of the wander azimuth angle (and heading). Once the heading of the INS has been observed, the system transitions to the navigation mode (system state=3) where the accelerometer and gyroscope errors are further refined using a small-angle model for the Kalman Filter. Both the rough alignment and the navigation modes implement GPS updates using a Kalman Filter. The state definitions in the rough alignment and navigation modes are shown below; the optional states 18-32 are available to estimate accelerometer and gyro scale-factor and misalignment errors if needed for a particular application, depending on the IMU used.

InterNav Kalman Filter States

Configurations Available

InterNav can be used on a variety of different host platforms and integrated with different GPS and inertial systems, including PC-104 or PCI-based single-board computers and standard Windows-based PC platforms. Any inertial sensor that provides DV/Dq measurements, and any GPS receiver that outputs pseudo-range and carrier-phase measurements, can be used for navigation. Contact us for more detailed information on embedding InterNav into your system.

InterNav Related Info