Aerospace Science and Technology
Reducing inertial navigation error using Tightly coupled integrated INS/GPS Structure

Amir Moghtadaei Rad

Volume 15, Issue 2 , October 2022, , Pages 47-60

https://doi.org/10.22034/jast.2022.306926.1099

Abstract
  Inertial navigation amplifies the noise of the input sensors over time due to the presence of an integrator in the output path to determine the position and attitude of the object. This system has high bandwidth and good short-term accuracy. On the other hand, GPS navigation has low bandwidth, low noise ...  Read More