Advanced Strapdown Inertial Navigation System
A sophisticated strapdown inertial navigation implementation integrating attitude, position, and velocity information with detailed algorithm descriptions
Explore MATLAB source code curated for "捷联惯导" with clean implementations, documentation, and examples.
A sophisticated strapdown inertial navigation implementation integrating attitude, position, and velocity information with detailed algorithm descriptions
MATLAB source code simulating aircraft attitude updates, focusing on strapdown inertial navigation system algorithms with implementation details for quaternion-based orientation calculations
This program suite consists of MATLAB implementations for strapdown inertial navigation algorithms based on quaternion method, featuring simulation programs for filter-based initial alignment, compass method initial alignment, strapdown inertial navigation solution, and integrated Kalman filtering, along with essential parameter matrix conversion utilities. All algorithms were developed through extensive research of classical strapdown navigation literature and have been thoroughly debugged. The results demonstrate conformance with Qin Yongyuan's "Inertial Navigation" textbook for cone error and sculling error calculations, ensuring high reliability. This suite is ideal for inertial navigation learners seeking reference implementations and improvement opportunities.
MATLAB-implemented strapdown inertial navigation initial alignment program featuring both moving base and stationary base alignment algorithms with comprehensive code documentation.
Integrated navigation program combining Strapdown INS and GPS, featuring initial alignment and filtering algorithms with practical code implementation details
MATLAB Code Implementation for Strapdown Inertial Navigation Solution with Sensor Data Processing and Algorithm Explanations
MATLAB Code Implementation of Kalman Filter with 15-Dimensional Navigation System Applications
INS Strapdown Inertial Navigation Solving Utilizing Fourth-Order Runge-Kutta Method for High-Precision Attitude Computation