A Simple Illustration of Simulink Sampling System
A straightforward demonstration of a Simulink sampling system with 0.1-second sampling period and zero-order hold implementation
Strapdown Inertial Navigation System Navigation Solution
Strapdown Inertial Navigation System Navigation Solution. Navigation computation using 600 seconds of north-oriented strapdown system data with constant flight altitude and 0.01s sampling period. Implementation involves attitude updating through quaternion integration and position calculation using velocity and acceleration data.