Aerospace and Electronic Systems Magazine August 2017 - 32
Inertial Navigation and Simultaneous Localization and Mapping
Figure 9.
a. The estimated x-axis accelerometer bias with uncertainty and b. x-axis gyroscope bias. Result of 12
Monte Carlo simulations.
32
IEEE A&E SYSTEMS MAGAZINE
AUGUST 2017
Table of Contents for the Digital Edition of Aerospace and Electronic Systems Magazine August 2017