Title :
Further results on "velocity/position integration formula (i): application to in-flight coarse alignment"
Author_Institution :
Sch. of Aeronaut. & Astronaut., Central South Univ., Changsha, China
Abstract :
This note improves upon our recent work [1] by effectively depressing the adverse effect of the lever arm on attitude estimation.
Keywords :
Global Positioning System; antennas; inertial navigation; attitude estimation; in-flight coarse alignment; lever arm; velocity/position integration formula; Antennas; Approximation methods; Estimation; Global Positioning System; Integral equations; Interference; Radar;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
DOI :
10.1109/TAES.2014.130212
