Navigation
Navigation software serves for calculation of coordinates of missiles based on IMU measurements and estimation of the influence of instrument errors on the error of coordinates.
Navigation software serves for calculation of coordinates of missiles based on IMU measurements and estimation of the influence of instrument errors on the error of coordinates.
Program name: | NavigSim – Navigation Simulation |
Version/Year: | Version 1.0, 2008. |
Capability: | Calculation of trajectory of flying vehicle based on data obtained from inertial measurement unit (IMU). Calculation of the dispersion od trajectory coordinates due to measurement errors. |
Purpose: | Determination of coordinates and orientation angles of a flying vehicle equipped with IMU in off-line mode. Examination of various integration methods on the accuracy of integration. Examination of measurement errors of gyros and accelerometers on the accuracy of determination of trajectory and angles. |
Method: | Numerical integration of navigation equations and angular position equations given specific forces and angular rates by IMU in time. Monte-Carlo simulation of the trajectory dispersion. |
Origin: | Original development based on published literature and own experience. |
Platform: | Windows XP, Vista, 7, 8, 8.1 and 10 |
Required software: | None |
Authors: | Dr Miodrag Curcin and Dr Danilo Cuk |
Download Presentation: | PDF PowerPoint |