INS (Inertial Navigation System) Toolbox for MATLAB®
The GPSoft INS Toolbox provides the necessary functions to emulate a wide variety of inertial sensors from RLGs and FOGs down to MEMS sensors via user-defined sensors errors such as biases, scale factor error and noise.
Version 3 of the INS Toolbox for MATLAB adds active flight control to the F-16 six degree-of-freedom (6DOF) trajectory generator. This addition greatly enhances the fidelity of the simulated trajectories as well as that of the simulated inertial sensor outputs. The toolbox contains functions that allow the user to define a dynamic trajectory in a local-level coordinate frame and then perform a full INS simulation in the rotating earth frame.
The INS Toolbox provides the necessary functions to emulate a wide variety of inertial sensors from RLG’s and FOG’s down to MEMS sensors via user-defined sensors errors such as biases, scale factor error and noise.
The INS Toolbox is fully compatible with the GPSoft SatNav Toolbox and both are utilized in GPSoft’s Navigation System Integration & Kalman Filter Toolbox.
All functions provided as ASCII M-files
All functions can be edited and modified by the user
210 page user manual included
Over two dozen example programs included
1 year of tech support from GPSoft!
Click here for examples of INS Toolbox analysis capabilities.
Related GNSS, INS and Kalman Courses
If you work with these MATLAB toolboxes, you may be interested in the following courses: