Abstract
There is much interest in integrated navigation using the Global Positioning System and Inertial Measurement Units. This integration combines the long-term accuracy of GPS with the short-term accuracy of IMUs, thereby realizing the best of both worlds. There is thus a need for realistic simulations of integrated GPS/IMU navigation systems. This paper discusses such a simulation and presents some simulation results. The specific application considered is missile navigation.
| Original language | American English |
|---|---|
| Journal | ISCA International Conference on Computer Applications in Industry and Engineering |
| State | Published - Dec 1 1993 |
Disciplines
- Electrical and Computer Engineering
- Navigation, Guidance, Control and Dynamics
- Systems and Communications
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