MATLAB Inertial Navigation Basic Algorithm Program

In the current version, the MATLAB inertial navigation basic algorithm program does not include extension functionality or interface control modules, which may restrict its flexibility and scalability in practical applications. The core implementation primarily consists of fundamental inertial navigation algorithms such as attitude update using direction cosine matrices or quaternions, velocity integration through mechanical arrangement equations, and position calculation via navigation frame transformation. Future versions will incorporate additional features and interface control programs to meet user requirements and enhance overall performance and usability. For instance, we plan to integrate new algorithms and modules supporting broader navigation applications including vehicle navigation and UAV navigation systems. These enhancements may involve implementing Kalman filter variants for sensor fusion, adding GPS/INS integration interfaces, and developing modular sensor calibration routines. Additionally, we will improve the program's interface and user experience by creating GUI components for parameter configuration, real-time data visualization tools, and simplified API calls for external system integration. Our ongoing development efforts focus on continuously refining the program to address user needs while advancing inertial navigation technology across various application domains.