Cart (Loading....) | Create Account
Close category search window
 

Attitude correction algorithm using GPS measurements for flight vehicles

Sign In

Cookies must be enabled to login.After enabling cookies , please use refresh or reload or ctrl+f5 on the browser for the login options.

Formats Non-Member Member
$31 $13
Learn how you can qualify for the best price for this item!
Become an IEEE Member or Subscribe to
IEEE Xplore for exclusive pricing!
close button

puzzle piece

IEEE membership options for an individual and IEEE Xplore subscriptions for an organization offer the most affordable access to essential journal articles, conference papers, standards, eBooks, and eLearning courses.

Learn more about:

IEEE membership

IEEE Xplore subscriptions

2 Author(s)
Kim, C.T. ; Sch. of Electron., Telecomm. & Comput. Eng., Hankuk Aviation Univ., Seoul, South Korea ; Kwag, Y.K.

For flight systems with an on-board seeker the attitude error is the major factor to determine the seeker pointing error at the time of object acquisition. To achieve a desired mission it must be minimized. The proposed algorithm corrects the attitude error in the guidance computer during flight by taking its position and velocity measurements from GPS or radar. This is possible since navigator's position and velocity states are correlated with attitude state. Computer simulation is shown to prove the proposed algorithm.

Published in:

Digital Avionics Systems Conference, 2002. Proceedings. The 21st  (Volume:2 )

Date of Conference:

2002

Need Help?


IEEE Advancing Technology for Humanity About IEEE Xplore | Contact | Help | Terms of Use | Nondiscrimination Policy | Site Map | Privacy & Opting Out of Cookies

A not-for-profit organization, IEEE is the world's largest professional association for the advancement of technology.
© Copyright 2014 IEEE - All rights reserved. Use of this web site signifies your agreement to the terms and conditions.