A Study on Aerodynamic Model Applied to Aiding Inertial Navigation System
碩士 === 中原大學 === 資訊工程研究所 === 83 === The main object of this paper describes a way to improve the precision of a hybrid inertial navigation system (INS) with aerodynamic model . A primitive hybird INS take advantage of global positio...
Main Authors: | , |
---|---|
Other Authors: | |
Format: | Others |
Language: | zh-TW |
Published: |
1995
|
Online Access: | http://ndltd.ncl.edu.tw/handle/86097435053893601461 |