Abstract
There is much interest in integrated navigation us- ing the Global Positioning System and Inertial Mea- surement Units (accelerometers and gyroscopes). The results reported in this paper quantify integrated nav- igation performance as a function of GPS receiver de- sign parameters. The specific application considered is missile navigation.
| Original language | American English |
|---|---|
| Journal | Proceedings of the 49th Annual Meeting of The Institute of Navigation |
| State | Published - Jun 1 1993 |
Disciplines
- Electrical and Computer Engineering
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