Inertial Navigation Transfer Alignment
Inertial navigation transfer alignment procedure, featuring velocity-plus-attitude alignment with sensor calibration algorithms
Application of Kalman Filtering in Navigation Solution Computation
This archive contains GPS measurement data simulation, inertial navigation solution computation, and implementation of Kalman filtering for navigation optimization
MATLAB Inertial Navigation Basic Algorithm Program
The MATLAB inertial navigation basic algorithm program currently lacks extension capabilities and interface control modules, limiting its practical application flexibility and scalability
MATLAB Inertial Navigation Toolbox with Installation Guide and User Manual
A comprehensive inertial navigation toolbox for MATLAB featuring installation instructions and user manual, providing simulation, analysis, and verification tools for inertial navigation systems with practical functions for attitude calculation, error analysis, and calibration procedures.
GPS Inertial Navigation Integration
GPS Inertial Navigation Integration (2nd Edition) by Chen Jun [Program Source Code Included] – Essential resource with practical algorithm implementations for navigation system development
GPS Inertial Navigation MATLAB Toolbox - MATLAB Source Code
MATLAB source code for GPS inertial navigation toolbox, ideal for beginners studying inertial navigation systems, facilitates mastery of INS/GPS integrated navigation techniques with practical implementation examples
gpsoft's Inertial Navigation Toolbox: A Comprehensive Development Toolkit
gpsoft's inertial navigation toolbox offers exceptional utility with robust features for navigation algorithm implementation and sensor data processing.
Inertial Navigation + GPS Integrated Navigation System
Inertial Navigation System (INS) and GPS integrated navigation, featuring classic algorithms with code implementation insights. Essential knowledge for navigation system developers.
Basic Inertial Navigation Simulation Program
Application Context: Inertial navigation uses inertial components (accelerometers) to measure the acceleration of a vehicle, then calculates velocity and position through integration and computation to achieve navigation and positioning. The components of an inertial navigation system are installed within the vehicle, operating without reliance on external information or energy radiation, making it resistant to interference and an autonomous navigation system. Key Technologies: Designed to understand fundamental principles of inertial navigation and perform simulations. Features efficient and practical code implementation with clear structure and comprehensive annotations. The simulation includes numerical integration algorithms (like Euler or Runge-Kutta methods) for motion trajectory calculation and coordinate transformation modules for navigation frame conversions.
Design and Implementation of a Simulation Platform for Aircraft Inertial Navigation Control Systems
Implementation Framework for an Aircraft Inertial Navigation Control System Design and Simulation Platform with Model-Based Development Support