Conventional avionic configurations for precision guided vehicles are often unnecessarily costly and inefficient because of built-in (but unused) redundancy in instrumentation attributed to the present day independent systems design approach. An integrated design approach using strapdown avionic components that has the potential for lowering cost, increasing reliability, and improving overall performance as a result of using fewer and less costly instruments in an efficient manner is described.
|Original language||English (US)|
|Number of pages||5|
|State||Published - Dec 1 1986|
All Science Journal Classification (ASJC) codes
- Computer Science Applications
- Electrical and Electronic Engineering