Figure 2 - uploaded by Salam Ismaeel
Content may be subject to copyright.
Download
View publication
2: Inertial and ECEF frames

2: Inertial and ECEF frames

Source publication
Figure 2.1: Missile coordinate systems
Figure 2.2: Inertial and ECEF frames
Figure 2.4: The simulation package of the hypothetical missile
Figure 3.4: Operational satellite constellation 
+4 Figure 3.3: GPS Major segments 
PhD Thesis, Al-Nahrain University
Article
Full-text available
  • Jun 2003
Strapdown inertial navigation systems (SDINS) are used for general navigation areas. Low cost inertial navigation systems (INSs) can cause large position errors in very short time, due to the low quality of the inertial measurement unit (IMU). On the other hand, the Global Positioning System (GPS) can accurately determine position, velocity, and ti...
Cite
Download full-text